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Passed
gpkit.tests.from_paths.TestFiles.test_solar_sens_chart_py_mosek (from gpkit.tests.from_paths.TestFiles-20180420145129)
Standard Output
Using solver 'mosek' Solving for 9073 variables. Solving took 2.75 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.3000 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 796269.5176 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 65.7609005055 ampere but the right hand side evaluated to 616.348265673 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.9%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 65.6904100315 ampere but the right hand side evaluated to 616.348266433 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 65.5943352119 ampere but the right hand side evaluated to 616.348267133 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 65.4468189041 ampere but the right hand side evaluated to 616.348267883 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 65.2157694838 ampere but the right hand side evaluated to 616.348268895 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 40.8361575014 volt but the right hand side evaluated to 40.0442877093 volt (Allowable error: 0.0001%, Actual error: 2%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 40.7564339544 volt but the right hand side evaluated to 40.0109034576 volt (Allowable error: 0.0001%, Actual error: 1.9%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 40.6357804503 volt but the right hand side evaluated to 39.9534916223 volt (Allowable error: 0.0001%, Actual error: 1.7%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 40.4485542327 volt but the right hand side evaluated to 39.8631072239 volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 40.1471960704 volt but the right hand side evaluated to 39.7128058563 volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 48.4046083817 ampere but the right hand side evaluated to 462.161099059 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 32.6524147448 volt but the right hand side evaluated to 32.6473131673 volt (Allowable error: 0.0001%, Actual error: 0.016%) Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.376958523 ampere but the right hand side evaluated to 461.909866954 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6357630197 volt but the right hand side evaluated to 32.63160971 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.4032724905 ampere but the right hand side evaluated to 462.148949629 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6515961471 volt but the right hand side evaluated to 32.6465395506 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.378977435 ampere but the right hand side evaluated to 461.928210077 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6369829574 volt but the right hand side evaluated to 32.6327603187 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.4012428858 ampere but the right hand side evaluated to 462.130502254 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6503693105 volt but the right hand side evaluated to 32.6453818662 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.3803022923 ampere but the right hand side evaluated to 461.940251653 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6377899459 volt but the right hand side evaluated to 32.6335221342 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.3985104692 ampere but the right hand side evaluated to 462.105681136 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6487388839 volt but the right hand side evaluated to 32.6438455983 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.3809332223 ampere but the right hand side evaluated to 461.945991596 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6381826286 volt but the right hand side evaluated to 32.6338937106 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.3950918511 ampere but the right hand side evaluated to 462.074619349 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.646685393 volt but the right hand side evaluated to 32.6419093832 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 48.3808926677 ampere but the right hand side evaluated to 461.945610865 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 32.6381385826 volt but the right hand side evaluated to 32.6338501389 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3909830891 ampere but the right hand side evaluated to 462.037282148 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6442062245 volt but the right hand side evaluated to 32.63957081 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3801430654 ampere but the right hand side evaluated to 461.938800856 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6376870464 volt but the right hand side evaluated to 32.6334243809 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3861615476 ampere but the right hand side evaluated to 461.993481418 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6413140224 volt but the right hand side evaluated to 32.636844619 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3786889425 ampere but the right hand side evaluated to 461.925595436 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6368188102 volt but the right hand side evaluated to 32.6326065284 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3806415653 ampere but the right hand side evaluated to 461.943330004 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6379872446 volt but the right hand side evaluated to 32.6337074769 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3765444482 ampere but the right hand side evaluated to 461.906106241 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6355147986 volt but the right hand side evaluated to 32.6313757624 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3744123365 ampere but the right hand side evaluated to 461.886735073 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6342252683 volt but the right hand side evaluated to 32.6301595323 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3736800771 ampere but the right hand side evaluated to 461.880088291 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6337931058 volt but the right hand side evaluated to 32.6297529209 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3674679674 ampere but the right hand side evaluated to 461.823643137 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6300216631 volt but the right hand side evaluated to 32.6261945657 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [A]... >= 9.55*i0_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3701100533 ampere but the right hand side evaluated to 461.847652734 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [V]... >= Kv_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6316318273 volt but the right hand side evaluated to 32.6277142553 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [A]... >= 9.55*i0_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3597904304 ampere but the right hand side evaluated to 461.753901062 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [v_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [V]... >= Kv_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.625379199 volt but the right hand side evaluated to 32.6218167526 volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [i_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3658230766 ampere but the right hand side evaluated to 461.808701505 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6290301166 volt but the right hand side evaluated to 32.6252596512 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3513889394 ampere but the right hand side evaluated to 461.677577486 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0096%) Warning: Constraint [v_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6202753777 volt but the right hand side evaluated to 32.6170021805 volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [i_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3608068102 ampere but the right hand side evaluated to 461.763127966 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6259866812 volt but the right hand side evaluated to 32.6223886798 volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [i_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3422456993 ampere but the right hand side evaluated to 461.594519551 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%) Warning: Constraint [v_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6147095652 volt but the right hand side evaluated to 32.6117514729 volt (Allowable error: 0.0001%, Actual error: 0.0091%) Warning: Constraint [i_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3550561028 ampere but the right hand side evaluated to 461.710882956 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0099%) Warning: Constraint [v_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6224922092 volt but the right hand side evaluated to 32.619091981 volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [i_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3323597498 ampere but the right hand side evaluated to 461.504711413 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0077%) Warning: Constraint [v_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6086649864 volt but the right hand side evaluated to 32.6060473637 volt (Allowable error: 0.0001%, Actual error: 0.008%) Warning: Constraint [i_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3485608055 ampere but the right hand side evaluated to 461.651875946 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0093%) Warning: Constraint [v_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6185403694 volt but the right hand side evaluated to 32.6153637329 volt (Allowable error: 0.0001%, Actual error: 0.0097%) Warning: Constraint [i_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3217150031 ampere but the right hand side evaluated to 461.408013287 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0066%) Warning: Constraint [v_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6021364126 volt but the right hand side evaluated to 32.5998856858 volt (Allowable error: 0.0001%, Actual error: 0.0069%) Warning: Constraint [i_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3413127552 ampere but the right hand side evaluated to 461.586032089 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%) Warning: Constraint [v_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6141214699 volt but the right hand side evaluated to 32.6111944761 volt (Allowable error: 0.0001%, Actual error: 0.009%) Warning: Constraint [i_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3103004186 ampere but the right hand side evaluated to 461.304325585 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0054%) Warning: Constraint [v_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5951124808 volt but the right hand side evaluated to 32.5932554868 volt (Allowable error: 0.0001%, Actual error: 0.0057%) Warning: Constraint [i_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.333301283 ampere but the right hand side evaluated to 461.513255209 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0078%) Warning: Constraint [v_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6092263179 volt but the right hand side evaluated to 32.6065754488 volt (Allowable error: 0.0001%, Actual error: 0.0081%) Warning: Constraint [i_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.2980770633 ampere but the right hand side evaluated to 461.193320677 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0042%) Warning: Constraint [v_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5876045768 volt but the right hand side evaluated to 32.586171416 volt (Allowable error: 0.0001%, Actual error: 0.0044%) Warning: Constraint [i_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3245063632 ampere but the right hand side evaluated to 461.433371495 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0069%) Warning: Constraint [v_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6038520194 volt but the right hand side evaluated to 32.6015050407 volt (Allowable error: 0.0001%, Actual error: 0.0072%) Warning: Constraint [i_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.2850803656 ampere but the right hand side evaluated to 461.075275971 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0029%) Warning: Constraint [v_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5795566285 volt but the right hand side evaluated to 32.5785729005 volt (Allowable error: 0.0001%, Actual error: 0.003%) Warning: Constraint [i_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3149434622 ampere but the right hand side evaluated to 461.346497074 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0059%) Warning: Constraint [v_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5979631541 volt but the right hand side evaluated to 32.5959455264 volt (Allowable error: 0.0001%, Actual error: 0.0062%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 but bound is 0.1460 Warning: Constraint [i_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.2712740105 ampere but the right hand side evaluated to 460.949883317 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0015%) Warning: Constraint [v_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5709738133 volt but the right hand side evaluated to 32.5704679549 volt (Allowable error: 0.0001%, Actual error: 0.0016%) Warning: Constraint [i_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3045581077 ampere but the right hand side evaluated to 461.25217492 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0049%) Warning: Constraint [v_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5915832004 volt but the right hand side evaluated to 32.5899250144 volt (Allowable error: 0.0001%, Actual error: 0.0051%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Warning: Constraint [i_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.2933606501 ampere but the right hand side evaluated to 461.150477076 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0037%) Warning: Constraint [v_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.584677047 volt but the right hand side evaluated to 32.5834064179 volt (Allowable error: 0.0001%, Actual error: 0.0039%) Using solver 'mosek' Solving for 9073 variables. Solving took 2 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2824 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 882794.0512 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1991 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0328 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0367 but bound is 0.0500 Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 83.6082501361 ampere but the right hand side evaluated to 779.784457036 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.4%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 83.5016049752 ampere but the right hand side evaluated to 779.78445709 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.3%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 83.3557342749 ampere but the right hand side evaluated to 779.784457139 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.1%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 83.1310518324 ampere but the right hand side evaluated to 779.78445719 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 82.7771607055 ampere but the right hand side evaluated to 779.78445726 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 38.5657784348 volt but the right hand side evaluated to 37.5903753645 volt (Allowable error: 0.0001%, Actual error: 2.6%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 38.4804161843 volt but the right hand side evaluated to 37.5596574844 volt (Allowable error: 0.0001%, Actual error: 2.5%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 38.3522610731 volt but the right hand side evaluated to 37.5062528295 volt (Allowable error: 0.0001%, Actual error: 2.3%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 38.1536666771 volt but the right hand side evaluated to 37.4222340767 volt (Allowable error: 0.0001%, Actual error: 2%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 37.8404671739 volt but the right hand side evaluated to 37.2880130212 volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [i_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [A]... >= 9.55*i0_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5643547165 ampere but the right hand side evaluated to 529.997456324 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [V]... >= Kv_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8016714064 volt but the right hand side evaluated to 34.7600660206 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [A]... >= 9.55*i0_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5215905091 ampere but the right hand side evaluated to 529.597242647 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [V]... >= Kv_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8064946635 volt but the right hand side evaluated to 34.7654161793 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [A]... >= 9.55*i0_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4297936903 ampere but the right hand side evaluated to 528.736313164 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [V]... >= Kv_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8139614785 volt but the right hand side evaluated to 34.7738930949 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [A]... >= 9.55*i0_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3865482317 ampere but the right hand side evaluated to 528.334967021 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [V]... >= Kv_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8251830415 volt but the right hand side evaluated to 34.7858768589 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [A]... >= 9.55*i0_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2803693726 ampere but the right hand side evaluated to 527.339737882 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [V]... >= Kv_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8358035223 volt but the right hand side evaluated to 34.797711553 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [A]... >= 9.55*i0_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2491924421 ampere but the right hand side evaluated to 527.050521106 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [V]... >= Kv_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8446142422 volt but the right hand side evaluated to 34.8070828827 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [A]... >= 9.55*i0_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1198991116 ampere but the right hand side evaluated to 525.841583904 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) Warning: Constraint [v_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [V]... >= Kv_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8644856605 volt but the right hand side evaluated to 34.8286409225 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [A]... >= 9.55*i0_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1083669037 ampere but the right hand side evaluated to 525.733352092 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) Warning: Constraint [v_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [V]... >= Kv_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8655615146 volt but the right hand side evaluated to 34.8298403774 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [A]... >= 9.55*i0_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9644157244 ampere but the right hand side evaluated to 524.386974572 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) Warning: Constraint [v_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [V]... >= Kv_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8887668818 volt but the right hand side evaluated to 34.8549077392 volt (Allowable error: 0.0001%, Actual error: 0.097%) Warning: Constraint [i_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [A]... >= 9.55*i0_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9628318135 ampere but the right hand side evaluated to 524.372071025 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) Warning: Constraint [v_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [V]... >= Kv_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8888551103 volt but the right hand side evaluated to 34.8550104357 volt (Allowable error: 0.0001%, Actual error: 0.097%) Warning: Constraint [i_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [A]... >= 9.55*i0_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.8041523031 ampere but the right hand side evaluated to 522.887320001 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) Warning: Constraint [v_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [V]... >= Kv_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9154329499 volt but the right hand side evaluated to 34.8836103376 volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [i_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [A]... >= 9.55*i0_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.8153896074 ampere but the right hand side evaluated to 522.991996182 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) Warning: Constraint [v_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [V]... >= Kv_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9124990764 volt but the right hand side evaluated to 34.8805007514 volt (Allowable error: 0.0001%, Actual error: 0.092%) Warning: Constraint [i_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [A]... >= 9.55*i0_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.6402494234 ampere but the right hand side evaluated to 521.352819871 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.081%) Warning: Constraint [v_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [V]... >= Kv_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9436464962 volt but the right hand side evaluated to 34.9138653969 volt (Allowable error: 0.0001%, Actual error: 0.085%) Warning: Constraint [i_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [A]... >= 9.55*i0_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.6618712957 ampere but the right hand side evaluated to 521.555064688 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.082%) Warning: Constraint [v_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [V]... >= Kv_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.939369086 volt but the right hand side evaluated to 34.9093052816 volt (Allowable error: 0.0001%, Actual error: 0.086%) Warning: Constraint [i_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [A]... >= 9.55*i0_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.4714788324 ampere but the right hand side evaluated to 519.772106502 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) Warning: Constraint [v_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [V]... >= Kv_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.974224993 volt but the right hand side evaluated to 34.946515392 volt (Allowable error: 0.0001%, Actual error: 0.079%) Warning: Constraint [i_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [A]... >= 9.55*i0_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.505572908 ampere but the right hand side evaluated to 520.091136006 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%) Warning: Constraint [v_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [V]... >= Kv_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9671230211 volt but the right hand side evaluated to 34.9389733979 volt (Allowable error: 0.0001%, Actual error: 0.081%) Warning: Constraint [i_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [A]... >= 9.55*i0_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.2975981942 ampere but the right hand side evaluated to 518.142749512 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.07%) Warning: Constraint [v_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [V]... >= Kv_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.007296087 volt but the right hand side evaluated to 34.9816808124 volt (Allowable error: 0.0001%, Actual error: 0.073%) Warning: Constraint [i_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [A]... >= 9.55*i0_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.3440884956 ampere but the right hand side evaluated to 518.578095245 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.071%) Warning: Constraint [v_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [V]... >= Kv_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.997402462 volt but the right hand side evaluated to 34.9712055143 volt (Allowable error: 0.0001%, Actual error: 0.075%) Warning: Constraint [i_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [A]... >= 9.55*i0_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.1178385958 ampere but the right hand side evaluated to 516.457465396 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%) Warning: Constraint [v_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [V]... >= Kv_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0433552112 volt but the right hand side evaluated to 35.0198619278 volt (Allowable error: 0.0001%, Actual error: 0.067%) Warning: Constraint [i_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [A]... >= 9.55*i0_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.1762495543 ampere but the right hand side evaluated to 517.005002853 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [v_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [V]... >= Kv_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0309835536 volt but the right hand side evaluated to 35.0067937026 volt (Allowable error: 0.0001%, Actual error: 0.069%) Warning: Constraint [i_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [A]... >= 9.55*i0_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.9307720132 ampere but the right hand side evaluated to 514.702838009 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.058%) Warning: Constraint [v_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [V]... >= Kv_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0833583727 volt but the right hand side evaluated to 35.0620309513 volt (Allowable error: 0.0001%, Actual error: 0.061%) Warning: Constraint [i_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [A]... >= 9.55*i0_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.0027375612 ampere but the right hand side evaluated to 515.377843599 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.06%) Warning: Constraint [v_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [V]... >= Kv_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0673494495 volt but the right hand side evaluated to 35.0451862309 volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [i_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [A]... >= 9.55*i0_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.7355628567 ampere but the right hand side evaluated to 512.870792448 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%) Warning: Constraint [v_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [V]... >= Kv_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1278482444 volt but the right hand side evaluated to 35.108725251 volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [i_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [A]... >= 9.55*i0_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.8220254586 ampere but the right hand side evaluated to 513.682294238 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%) Warning: Constraint [v_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [V]... >= Kv_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1075263661 volt but the right hand side evaluated to 35.0874280982 volt (Allowable error: 0.0001%, Actual error: 0.057%) Warning: Constraint [i_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [A]... >= 9.55*i0_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.5316994218 ampere but the right hand side evaluated to 510.956171515 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.046%) Warning: Constraint [v_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [V]... >= Kv_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1771423516 volt but the right hand side evaluated to 35.1602448104 volt (Allowable error: 0.0001%, Actual error: 0.048%) Warning: Constraint [i_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [A]... >= 9.55*i0_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.633620409 ampere but the right hand side evaluated to 511.91345999 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.049%) Warning: Constraint [v_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [V]... >= Kv_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1518182971 volt but the right hand side evaluated to 35.133811349 volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [i_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [A]... >= 9.55*i0_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.3157432977 ampere but the right hand side evaluated to 508.926604144 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.04%) Warning: Constraint [v_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [V]... >= Kv_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.233607074 volt but the right hand side evaluated to 35.218990035 volt (Allowable error: 0.0001%, Actual error: 0.042%) Warning: Constraint [i_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [A]... >= 9.55*i0_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.4353998876 ampere but the right hand side evaluated to 510.051299648 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.043%) Warning: Constraint [v_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [V]... >= Kv_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.2016698189 volt but the right hand side evaluated to 35.1857977221 volt (Allowable error: 0.0001%, Actual error: 0.045%) Warning: Constraint [i_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [A]... >= 9.55*i0_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.0857762944 ampere but the right hand side evaluated to 506.763516375 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.033%) Warning: Constraint [v_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [V]... >= Kv_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.2985535803 volt but the right hand side evaluated to 35.286256199 volt (Allowable error: 0.0001%, Actual error: 0.035%) Warning: Constraint [i_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [A]... >= 9.55*i0_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.2255177789 ampere but the right hand side evaluated to 508.07813661 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.037%) Warning: Constraint [v_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [V]... >= Kv_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.25833582 volt but the right hand side evaluated to 35.2446404687 volt (Allowable error: 0.0001%, Actual error: 0.039%) Warning: Constraint [i_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [A]... >= 9.55*i0_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.8375034196 ampere but the right hand side evaluated to 504.425911817 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [v_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [V]... >= Kv_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.3749666968 volt but the right hand side evaluated to 35.3650319103 volt (Allowable error: 0.0001%, Actual error: 0.028%) Warning: Constraint [i_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [A]... >= 9.55*i0_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.0011118134 ampere but the right hand side evaluated to 505.966632866 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.031%) Warning: Constraint [v_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [V]... >= Kv_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.3237883732 volt but the right hand side evaluated to 35.3123133102 volt (Allowable error: 0.0001%, Actual error: 0.032%) Warning: Constraint [i_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [A]... >= 9.55*i0_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.563700871 ampere but the right hand side evaluated to 501.844822711 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.02%) Warning: Constraint [v_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [V]... >= Kv_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.4679071128 volt but the right hand side evaluated to 35.4603822977 volt (Allowable error: 0.0001%, Actual error: 0.021%) Warning: Constraint [i_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [A]... >= 9.55*i0_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.7581499005 ampere but the right hand side evaluated to 503.678195045 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.025%) Warning: Constraint [v_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [V]... >= Kv_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.400830603 volt but the right hand side evaluated to 35.3916154803 volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [i_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [A]... >= 9.55*i0_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.2509579596 ampere but the right hand side evaluated to 498.892089797 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [V]... >= Kv_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.5868288423 volt but the right hand side evaluated to 35.5817592518 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [A]... >= 9.55*i0_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.4890816267 ampere but the right hand side evaluated to 501.14074064 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.019%) Warning: Constraint [v_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [V]... >= Kv_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.4947553429 volt but the right hand side evaluated to 35.4878444212 volt (Allowable error: 0.0001%, Actual error: 0.019%) Warning: Constraint [i_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [A]... >= 9.55*i0_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.86390163 ampere but the right hand side evaluated to 495.229870921 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0068%) Warning: Constraint [v_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [V]... >= Kv_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.756772671 volt but the right hand side evaluated to 35.7542076311 volt (Allowable error: 0.0001%, Actual error: 0.0072%) Warning: Constraint [i_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [A]... >= 9.55*i0_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.1785642518 ampere but the right hand side evaluated to 498.207800498 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [V]... >= Kv_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.6163802771 volt but the right hand side evaluated to 35.6118258513 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1991 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0328 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0367 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1991 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0328 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0367 but bound is 0.0500 Using solver 'mosek' Solving for 9073 variables. Solving took 2.3 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2351 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 988744.2411 but bound is 600000.0000 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2106 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0340 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0369 but bound is 0.0500 Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 99.8053665527 ampere but the right hand side evaluated to 936.513511236 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 99.7125436974 ampere but the right hand side evaluated to 936.513511243 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 99.586600469 ampere but the right hand side evaluated to 936.513511252 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 99.3939698935 ampere but the right hand side evaluated to 936.513511258 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 99.0931287278 ampere but the right hand side evaluated to 936.513511269 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 38.2500478044 volt but the right hand side evaluated to 37.5140775039 volt (Allowable error: 0.0001%, Actual error: 2%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 38.1813138061 volt but the right hand side evaluated to 37.4858738795 volt (Allowable error: 0.0001%, Actual error: 1.9%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 38.0772361466 volt but the right hand side evaluated to 37.4367677753 volt (Allowable error: 0.0001%, Actual error: 1.7%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 37.9163410431 volt but the right hand side evaluated to 37.3595016651 volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 37.6635831337 volt but the right hand side evaluated to 37.236168007 volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [A]... >= 9.55*i0_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.8562215351 ampere but the right hand side evaluated to 627.638333336 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [V]... >= Kv_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0193095114 volt but the right hand side evaluated to 34.9458478712 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [A]... >= 9.55*i0_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.8479913174 ampere but the right hand side evaluated to 627.558656574 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [V]... >= Kv_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0179368132 volt but the right hand side evaluated to 34.9444051704 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [A]... >= 9.55*i0_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.5672494796 ampere but the right hand side evaluated to 624.946002356 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [V]... >= Kv_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0396670695 volt but the right hand side evaluated to 34.9698517518 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [A]... >= 9.55*i0_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.5696397725 ampere but the right hand side evaluated to 624.963584909 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [V]... >= Kv_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0363821042 volt but the right hand side evaluated to 34.9662638842 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [A]... >= 9.55*i0_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.2731994905 ampere but the right hand side evaluated to 622.207809132 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [V]... >= Kv_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0630821893 volt but the right hand side evaluated to 34.9970940042 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [A]... >= 9.55*i0_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.2860176722 ampere but the right hand side evaluated to 622.321267294 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [V]... >= Kv_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0579710451 volt but the right hand side evaluated to 34.9914701765 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [A]... >= 9.55*i0_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.9803638959 ampere but the right hand side evaluated to 619.476638201 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [V]... >= Kv_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.085271093 volt but the right hand side evaluated to 35.0228761189 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [A]... >= 9.55*i0_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.0010582089 ampere but the right hand side evaluated to 619.664498472 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [V]... >= Kv_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0799879539 volt but the right hand side evaluated to 35.0170355183 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [A]... >= 9.55*i0_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.6877567431 ampere but the right hand side evaluated to 616.744243231 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [V]... >= Kv_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1068155261 volt but the right hand side evaluated to 35.0478445514 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [A]... >= 9.55*i0_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.7128698064 ampere but the right hand side evaluated to 616.976997702 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [V]... >= Kv_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1036069599 volt but the right hand side evaluated to 35.0442373332 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [A]... >= 9.55*i0_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.3852325919 ampere but the right hand side evaluated to 613.92362267 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [V]... >= Kv_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.134355185 volt but the right hand side evaluated to 35.079216636 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [A]... >= 9.55*i0_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.4226778331 ampere but the right hand side evaluated to 614.268957367 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [V]... >= Kv_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1279305164 volt but the right hand side evaluated to 35.072090515 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [A]... >= 9.55*i0_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.0818778278 ampere but the right hand side evaluated to 611.091990606 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [V]... >= Kv_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1617694909 volt but the right hand side evaluated to 35.1103151712 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [A]... >= 9.55*i0_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.1264193784 ampere but the right hand side evaluated to 611.5051871 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [V]... >= Kv_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1555600405 volt but the right hand side evaluated to 35.1034089568 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [A]... >= 9.55*i0_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 63.7762695396 ampere but the right hand side evaluated to 608.237018747 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [V]... >= Kv_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1899182141 volt but the right hand side evaluated to 35.1420726802 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [A]... >= 9.55*i0_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 63.8267917834 ampere but the right hand side evaluated to 608.708418919 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [V]... >= Kv_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1846203417 volt but the right hand side evaluated to 35.1361412482 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [A]... >= 9.55*i0_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 63.4629766511 ampere but the right hand side evaluated to 605.311285206 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [V]... >= Kv_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.2222934966 volt but the right hand side evaluated to 35.1782462829 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [A]... >= 9.55*i0_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 63.5245935112 ampere but the right hand side evaluated to 605.885310138 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [V]... >= Kv_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 35.2144993589 volt but the right hand side evaluated to 35.169617842 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [A]... >= 9.55*i0_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 63.1454823017 ampere but the right hand side evaluated to 602.344448806 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [V]... >= Kv_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 35.2565026349 volt but the right hand side evaluated to 35.2162307818 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [A]... >= 9.55*i0_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 63.214783932 ampere but the right hand side evaluated to 602.991662685 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [V]... >= Kv_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 35.2484290878 volt but the right hand side evaluated to 35.2073068519 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [A]... >= 9.55*i0_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.8221043508 ampere but the right hand side evaluated to 599.321391909 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) Warning: Constraint [v_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [V]... >= Kv_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.2935607932 volt but the right hand side evaluated to 35.2570991711 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [A]... >= 9.55*i0_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.9011824588 ampere but the right hand side evaluated to 600.060249433 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [V]... >= Kv_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.2838034205 volt but the right hand side evaluated to 35.2463821441 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [A]... >= 9.55*i0_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.4925674046 ampere but the right hand side evaluated to 596.239163505 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) Warning: Constraint [v_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [V]... >= Kv_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.333555297 volt but the right hand side evaluated to 35.3009209572 volt (Allowable error: 0.0001%, Actual error: 0.092%) Warning: Constraint [i_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [A]... >= 9.55*i0_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.5797041061 ampere but the right hand side evaluated to 597.054794143 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.09%) Warning: Constraint [v_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [V]... >= Kv_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.3232150509 volt but the right hand side evaluated to 35.2896029284 volt (Allowable error: 0.0001%, Actual error: 0.095%) Warning: Constraint [i_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [A]... >= 9.55*i0_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.1579158283 ampere but the right hand side evaluated to 593.106501301 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%) Warning: Constraint [v_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [V]... >= Kv_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.3757102557 volt but the right hand side evaluated to 35.3468457245 volt (Allowable error: 0.0001%, Actual error: 0.082%) Warning: Constraint [i_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [A]... >= 9.55*i0_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.2517354433 ampere but the right hand side evaluated to 593.986843343 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [v_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [V]... >= Kv_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.3656596007 volt but the right hand side evaluated to 35.3358642119 volt (Allowable error: 0.0001%, Actual error: 0.084%) Warning: Constraint [i_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [A]... >= 9.55*i0_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.806793222 ampere but the right hand side evaluated to 589.821788997 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [v_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [V]... >= Kv_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.4273542698 volt but the right hand side evaluated to 35.4026266949 volt (Allowable error: 0.0001%, Actual error: 0.07%) Warning: Constraint [i_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [A]... >= 9.55*i0_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.915757072 ampere but the right hand side evaluated to 590.842333692 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.069%) Warning: Constraint [v_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [V]... >= Kv_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.4120389867 volt but the right hand side evaluated to 35.3860971056 volt (Allowable error: 0.0001%, Actual error: 0.073%) Warning: Constraint [i_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [A]... >= 9.55*i0_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.4495417765 ampere but the right hand side evaluated to 586.475879466 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%) Warning: Constraint [v_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [V]... >= Kv_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.4816257653 volt but the right hand side evaluated to 35.4609176344 volt (Allowable error: 0.0001%, Actual error: 0.058%) Warning: Constraint [i_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [A]... >= 9.55*i0_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.5712475457 ampere but the right hand side evaluated to 587.61589472 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.059%) Warning: Constraint [v_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [V]... >= Kv_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.4625994225 volt but the right hand side evaluated to 35.4405259079 volt (Allowable error: 0.0001%, Actual error: 0.062%) Warning: Constraint [i_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [A]... >= 9.55*i0_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.0866663498 ampere but the right hand side evaluated to 583.072866746 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.045%) Warning: Constraint [v_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [V]... >= Kv_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.538106568 volt but the right hand side evaluated to 35.5212533586 volt (Allowable error: 0.0001%, Actual error: 0.047%) Warning: Constraint [i_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [A]... >= 9.55*i0_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.2164351004 ampere but the right hand side evaluated to 584.2908523 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.048%) Warning: Constraint [v_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [V]... >= Kv_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.5184021741 volt but the right hand side evaluated to 35.5002296955 volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [i_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [A]... >= 9.55*i0_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 60.7005544387 ampere but the right hand side evaluated to 579.453010675 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.034%) Warning: Constraint [v_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [V]... >= Kv_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.6081765134 volt but the right hand side evaluated to 35.5955521605 volt (Allowable error: 0.0001%, Actual error: 0.035%) Warning: Constraint [i_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [A]... >= 9.55*i0_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 60.8482210985 ampere but the right hand side evaluated to 580.838257055 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [V]... >= Kv_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.5813694136 volt but the right hand side evaluated to 35.5671747966 volt (Allowable error: 0.0001%, Actual error: 0.04%) Warning: Constraint [i_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [A]... >= 9.55*i0_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 60.3007127041 ampere but the right hand side evaluated to 575.700001852 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.022%) Warning: Constraint [v_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [V]... >= Kv_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.6855319219 volt but the right hand side evaluated to 35.6770671144 volt (Allowable error: 0.0001%, Actual error: 0.024%) Warning: Constraint [i_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [A]... >= 9.55*i0_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 60.4639074713 ampere but the right hand side evaluated to 577.232228207 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [v_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [V]... >= Kv_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.6531550472 volt but the right hand side evaluated to 35.6430131217 volt (Allowable error: 0.0001%, Actual error: 0.028%) Warning: Constraint [i_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [A]... >= 9.55*i0_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8791609332 ampere but the right hand side evaluated to 571.739266548 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [V]... >= Kv_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.7752527497 volt but the right hand side evaluated to 35.7709879609 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [A]... >= 9.55*i0_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 60.0608454758 ampere but the right hand side evaluated to 573.44677771 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.016%) Warning: Constraint [v_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [V]... >= Kv_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.7353731495 volt but the right hand side evaluated to 35.7293202128 volt (Allowable error: 0.0001%, Actual error: 0.017%) Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2106 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0340 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0369 but bound is 0.0500 Warning: Constraint [i_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [A]... >= 9.55*i0_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6316175062 ampere but the right hand side evaluated to 569.411442625 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.005%) Warning: Constraint [v_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [V]... >= Kv_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.832710034 volt but the right hand side evaluated to 35.8308142901 volt (Allowable error: 0.0001%, Actual error: 0.0053%) Using solver 'mosek' Solving for 4713 variables. Solving took 1.06 seconds. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.2058 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1064456.8435 but bound is 600000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 111.917810713 ampere but the right hand side evaluated to 1056.06638268 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 111.846541257 ampere but the right hand side evaluated to 1056.06638269 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 111.750519055 ampere but the right hand side evaluated to 1056.0663827 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 111.604592276 ampere but the right hand side evaluated to 1056.06638272 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 111.378510957 ampere but the right hand side evaluated to 1056.06638273 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 38.2100218668 volt but the right hand side evaluated to 37.7037019531 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 38.1552399 volt but the right hand side evaluated to 37.6768755058 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 38.0707771602 volt but the right hand side evaluated to 37.630062704 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 37.9401425879 volt but the right hand side evaluated to 37.5563497138 volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 37.7350477929 volt but the right hand side evaluated to 37.4386740022 volt (Allowable error: 0.0001%, Actual error: 0.79%) Warning: Constraint [i_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [A]... >= 9.55*i0_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 73.3931414697 ampere but the right hand side evaluated to 699.26296302 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [V]... >= Kv_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.2475642196 volt but the right hand side evaluated to 35.1620428599 volt (Allowable error: 0.0001%, Actual error: 0.24%) Warning: Constraint [i_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [A]... >= 9.55*i0_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 73.0289058934 ampere but the right hand side evaluated to 695.876983177 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [V]... >= Kv_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.2658446392 volt but the right hand side evaluated to 35.1848748505 volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [i_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [A]... >= 9.55*i0_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 72.6669896055 ampere but the right hand side evaluated to 692.506049518 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [V]... >= Kv_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.2825857881 volt but the right hand side evaluated to 35.2058330309 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [A]... >= 9.55*i0_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 72.3031326078 ampere but the right hand side evaluated to 689.116210078 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [V]... >= Kv_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.3004820175 volt but the right hand side evaluated to 35.2279643094 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [A]... >= 9.55*i0_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 71.9369645103 ampere but the right hand side evaluated to 685.704028273 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [V]... >= Kv_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.3196517498 volt but the right hand side evaluated to 35.251393136 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [A]... >= 9.55*i0_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 71.569996075 ampere but the right hand side evaluated to 682.281341155 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [V]... >= Kv_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.3389918789 volt but the right hand side evaluated to 35.2748778148 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [A]... >= 9.55*i0_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 71.1963086389 ampere but the right hand side evaluated to 678.799478768 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [V]... >= Kv_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.3622192681 volt but the right hand side evaluated to 35.302558772 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [A]... >= 9.55*i0_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 70.8211720807 ampere but the right hand side evaluated to 675.300815276 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [V]... >= Kv_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.385790114 volt but the right hand side evaluated to 35.3304652137 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [A]... >= 9.55*i0_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 70.4426766308 ampere but the right hand side evaluated to 671.769302015 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [V]... >= Kv_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.4108203797 volt but the right hand side evaluated to 35.3598315695 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [A]... >= 9.55*i0_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 70.0648709307 ampere but the right hand side evaluated to 668.238307761 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [V]... >= Kv_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.4345972488 volt but the right hand side evaluated to 35.3876533127 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [A]... >= 9.55*i0_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 69.6718344631 ampere but the right hand side evaluated to 664.574165758 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [V]... >= Kv_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.4671817665 volt but the right hand side evaluated to 35.4250080041 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [A]... >= 9.55*i0_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 69.2794499924 ampere but the right hand side evaluated to 660.909016887 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [V]... >= Kv_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.4982825422 volt but the right hand side evaluated to 35.4605262938 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [A]... >= 9.55*i0_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 68.8780417025 ampere but the right hand side evaluated to 657.160735543 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%) Warning: Constraint [v_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [V]... >= Kv_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.5339390198 volt but the right hand side evaluated to 35.5008211904 volt (Allowable error: 0.0001%, Actual error: 0.093%) Warning: Constraint [i_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [A]... >= 9.55*i0_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 68.4705014199 ampere but the right hand side evaluated to 653.352897113 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) Warning: Constraint [v_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [V]... >= Kv_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.5721736181 volt but the right hand side evaluated to 35.5436916655 volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [i_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [A]... >= 9.55*i0_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 68.0565748959 ampere but the right hand side evaluated to 649.482597561 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [v_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [V]... >= Kv_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.6130141687 volt but the right hand side evaluated to 35.5891398005 volt (Allowable error: 0.0001%, Actual error: 0.067%) Warning: Constraint [i_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [A]... >= 9.55*i0_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 67.6342938152 ampere but the right hand side evaluated to 645.53201312 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [V]... >= Kv_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.6575621906 volt but the right hand side evaluated to 35.6383246653 volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [i_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [A]... >= 9.55*i0_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 67.2008049908 ampere but the right hand side evaluated to 641.475148139 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [V]... >= Kv_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.7074556611 volt but the right hand side evaluated to 35.6929605185 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [A]... >= 9.55*i0_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 66.7560125597 ampere but the right hand side evaluated to 637.309632528 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [V]... >= Kv_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.762587156 volt but the right hand side evaluated to 35.7528599036 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [A]... >= 9.55*i0_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 66.2964788144 ampere but the right hand side evaluated to 633.003357774 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [V]... >= Kv_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.8249152363 volt but the right hand side evaluated to 35.8200288692 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 9073 variables. Solving took 1.81 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.3000 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 796269.5178 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 65.7608999693 ampere but the right hand side evaluated to 616.348267117 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.9%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 65.6904096557 ampere but the right hand side evaluated to 616.348267878 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 65.5943350322 ampere but the right hand side evaluated to 616.348268579 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 65.446818975 ampere but the right hand side evaluated to 616.348269331 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 65.2157698202 ampere but the right hand side evaluated to 616.348270344 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 40.8361570363 volt but the right hand side evaluated to 40.044287691 volt (Allowable error: 0.0001%, Actual error: 2%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 40.7564335984 volt but the right hand side evaluated to 40.0109034446 volt (Allowable error: 0.0001%, Actual error: 1.9%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 40.6357802279 volt but the right hand side evaluated to 39.9534916159 volt (Allowable error: 0.0001%, Actual error: 1.7%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 40.4485541808 volt but the right hand side evaluated to 39.8631072259 volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 40.1471961991 volt but the right hand side evaluated to 39.7128058672 volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 48.4046054847 ampere but the right hand side evaluated to 462.161071357 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 32.6524167507 volt but the right hand side evaluated to 32.6473151699 volt (Allowable error: 0.0001%, Actual error: 0.016%) Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.3769561686 ampere but the right hand side evaluated to 461.90984445 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.635764662 volt but the right hand side evaluated to 32.6316113501 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.4032696193 ampere but the right hand side evaluated to 462.148922175 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6515981362 volt but the right hand side evaluated to 32.6465415366 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.3789750409 ampere but the right hand side evaluated to 461.928187193 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6369846264 volt but the right hand side evaluated to 32.6327619854 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.4012400541 ampere but the right hand side evaluated to 462.130475179 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6503712734 volt but the right hand side evaluated to 32.6453838263 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.3802998726 ampere but the right hand side evaluated to 461.940228523 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6377916319 volt but the right hand side evaluated to 32.6335238179 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.3985076922 ampere but the right hand side evaluated to 462.105654582 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6487408101 volt but the right hand side evaluated to 32.6438475218 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.3809307917 ampere but the right hand side evaluated to 461.94596836 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6381843217 volt but the right hand side evaluated to 32.6338954013 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 48.3950891412 ampere but the right hand side evaluated to 462.074593438 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 32.6466872742 volt but the right hand side evaluated to 32.6419112618 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 48.3808902371 ampere but the right hand side evaluated to 461.945587629 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 32.6381402759 volt but the right hand side evaluated to 32.6338518301 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3909804596 ampere but the right hand side evaluated to 462.037257007 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6442080519 volt but the right hand side evaluated to 32.6395726351 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3801406503 ampere but the right hand side evaluated to 461.938777768 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6376887293 volt but the right hand side evaluated to 32.6334260617 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3861590133 ampere but the right hand side evaluated to 461.993457187 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6413157857 volt but the right hand side evaluated to 32.63684638 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3786865577 ampere but the right hand side evaluated to 461.925572636 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6368204727 volt but the right hand side evaluated to 32.6326081888 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3806391398 ampere but the right hand side evaluated to 461.943306814 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6379889347 volt but the right hand side evaluated to 32.633709165 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3765421064 ampere but the right hand side evaluated to 461.906083852 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6355164323 volt but the right hand side evaluated to 32.6313773941 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3744100341 ampere but the right hand side evaluated to 461.886713061 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6342268759 volt but the right hand side evaluated to 32.6301611382 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3736777936 ampere but the right hand side evaluated to 461.880066457 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6337947002 volt but the right hand side evaluated to 32.6297545135 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3674658021 ampere but the right hand side evaluated to 461.823622437 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6300231787 volt but the right hand side evaluated to 32.6261960798 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [A]... >= 9.55*i0_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3701078413 ampere but the right hand side evaluated to 461.847631584 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [V]... >= Kv_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6316333738 volt but the right hand side evaluated to 32.6277158 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [A]... >= 9.55*i0_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3597884166 ampere but the right hand side evaluated to 461.753881808 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [v_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [V]... >= Kv_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.625380612 volt but the right hand side evaluated to 32.621818164 volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [i_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3658209518 ampere but the right hand side evaluated to 461.80868118 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6290316027 volt but the right hand side evaluated to 32.6252611351 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3513870924 ampere but the right hand side evaluated to 461.67755983 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0096%) Warning: Constraint [v_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6202766788 volt but the right hand side evaluated to 32.6170034803 volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [i_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3608047819 ampere but the right hand side evaluated to 461.763108574 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6259881045 volt but the right hand side evaluated to 32.6223901018 volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [i_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3422440335 ampere but the right hand side evaluated to 461.594503627 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%) Warning: Constraint [v_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6147107441 volt but the right hand side evaluated to 32.6117526502 volt (Allowable error: 0.0001%, Actual error: 0.0091%) Warning: Constraint [i_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3550541894 ampere but the right hand side evaluated to 461.710864653 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0099%) Warning: Constraint [v_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6224935537 volt but the right hand side evaluated to 32.6190933236 volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [i_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3323582779 ampere but the right hand side evaluated to 461.504697349 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0077%) Warning: Constraint [v_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6086660356 volt but the right hand side evaluated to 32.6060484114 volt (Allowable error: 0.0001%, Actual error: 0.008%) Warning: Constraint [i_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3485590198 ampere but the right hand side evaluated to 461.651858865 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0093%) Warning: Constraint [v_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6185416279 volt but the right hand side evaluated to 32.6153649897 volt (Allowable error: 0.0001%, Actual error: 0.0097%) Warning: Constraint [i_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.321713747 ampere but the right hand side evaluated to 461.408001264 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0066%) Warning: Constraint [v_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6021373133 volt but the right hand side evaluated to 32.5998865834 volt (Allowable error: 0.0001%, Actual error: 0.0069%) Warning: Constraint [i_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3413111123 ampere but the right hand side evaluated to 461.586016371 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%) Warning: Constraint [v_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6141226322 volt but the right hand side evaluated to 32.6111956369 volt (Allowable error: 0.0001%, Actual error: 0.009%) Warning: Constraint [i_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3102993918 ampere but the right hand side evaluated to 461.304315738 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0054%) Warning: Constraint [v_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5951132247 volt but the right hand side evaluated to 32.593256227 volt (Allowable error: 0.0001%, Actual error: 0.0057%) Warning: Constraint [i_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3332997978 ampere but the right hand side evaluated to 461.513240995 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0078%) Warning: Constraint [v_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6092273737 volt but the right hand side evaluated to 32.6065765032 volt (Allowable error: 0.0001%, Actual error: 0.0081%) Warning: Constraint [i_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.2980762751 ampere but the right hand side evaluated to 461.193313146 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0042%) Warning: Constraint [v_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5876051649 volt but the right hand side evaluated to 32.5861720034 volt (Allowable error: 0.0001%, Actual error: 0.0044%) Warning: Constraint [i_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3245050505 ampere but the right hand side evaluated to 461.433358947 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0069%) Warning: Constraint [v_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.6038529618 volt but the right hand side evaluated to 32.6015059829 volt (Allowable error: 0.0001%, Actual error: 0.0072%) Warning: Constraint [i_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.285079839 ampere but the right hand side evaluated to 461.075270939 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0029%) Warning: Constraint [v_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5795570403 volt but the right hand side evaluated to 32.5785733117 volt (Allowable error: 0.0001%, Actual error: 0.003%) Warning: Constraint [i_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3149423442 ampere but the right hand side evaluated to 461.346486363 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0059%) Warning: Constraint [v_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5979639618 volt but the right hand side evaluated to 32.5959463323 volt (Allowable error: 0.0001%, Actual error: 0.0062%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 but bound is 0.1460 Warning: Constraint [i_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.271273773 ampere but the right hand side evaluated to 460.949881045 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0015%) Warning: Constraint [v_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5709740291 volt but the right hand side evaluated to 32.5704681704 volt (Allowable error: 0.0001%, Actual error: 0.0016%) Warning: Constraint [i_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.3045571953 ampere but the right hand side evaluated to 461.25216619 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0049%) Warning: Constraint [v_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5915838727 volt but the right hand side evaluated to 32.589925686 volt (Allowable error: 0.0001%, Actual error: 0.0051%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500 Warning: Constraint [i_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.2933599618 ampere but the right hand side evaluated to 461.150470497 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0037%) Warning: Constraint [v_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5846775692 volt but the right hand side evaluated to 32.5834069402 volt (Allowable error: 0.0001%, Actual error: 0.0039%) Using solver 'mosek' Solving for 9073 variables. Solving took 1.87 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2824 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 882794.0256 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1991 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0328 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0367 but bound is 0.0500 Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 83.6084089073 ampere but the right hand side evaluated to 779.784421752 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.4%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 83.5017269734 ampere but the right hand side evaluated to 779.784421755 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.3%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 83.3558110326 ampere but the right hand side evaluated to 779.784421757 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.1%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 83.1310704264 ampere but the right hand side evaluated to 779.78442176 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 82.7771166435 ampere but the right hand side evaluated to 779.784421764 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 38.5658652477 volt but the right hand side evaluated to 37.5903793532 volt (Allowable error: 0.0001%, Actual error: 2.6%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 38.4804829835 volt but the right hand side evaluated to 37.5596602597 volt (Allowable error: 0.0001%, Actual error: 2.5%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 38.352303314 volt but the right hand side evaluated to 37.5062541098 volt (Allowable error: 0.0001%, Actual error: 2.3%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 38.1536775123 volt but the right hand side evaluated to 37.4222334366 volt (Allowable error: 0.0001%, Actual error: 2%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 37.8404447263 volt but the right hand side evaluated to 37.288010317 volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [i_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [A]... >= 9.55*i0_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5657294661 ampere but the right hand side evaluated to 530.010860525 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [V]... >= Kv_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8008471031 volt but the right hand side evaluated to 34.7592625797 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [A]... >= 9.55*i0_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5229512931 ampere but the right hand side evaluated to 529.610507725 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [V]... >= Kv_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8056775579 volt but the right hand side evaluated to 34.7646195237 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [A]... >= 9.55*i0_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4293437589 ampere but the right hand side evaluated to 528.73317077 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [V]... >= Kv_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8144007669 volt but the right hand side evaluated to 34.7744114411 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [A]... >= 9.55*i0_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.387880013 ampere but the right hand side evaluated to 528.347926319 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [V]... >= Kv_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8243776931 volt but the right hand side evaluated to 34.7850899168 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [A]... >= 9.55*i0_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.280060757 ampere but the right hand side evaluated to 527.337797523 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [V]... >= Kv_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8361348864 volt but the right hand side evaluated to 34.7981122349 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [A]... >= 9.55*i0_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.250492372 ampere but the right hand side evaluated to 527.063149767 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [V]... >= Kv_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8438227956 volt but the right hand side evaluated to 34.8063079474 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [A]... >= 9.55*i0_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1211535218 ampere but the right hand side evaluated to 525.85376041 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) Warning: Constraint [v_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [V]... >= Kv_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8637181917 volt but the right hand side evaluated to 34.8278886675 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [A]... >= 9.55*i0_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1096352632 ampere but the right hand side evaluated to 525.745652572 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.097%) Warning: Constraint [v_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [V]... >= Kv_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8647837669 volt but the right hand side evaluated to 34.8290772249 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [A]... >= 9.55*i0_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9656195189 ampere but the right hand side evaluated to 524.398646208 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) Warning: Constraint [v_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [V]... >= Kv_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8880257575 volt but the right hand side evaluated to 34.8541802444 volt (Allowable error: 0.0001%, Actual error: 0.097%) Warning: Constraint [i_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [A]... >= 9.55*i0_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9640291708 ampere but the right hand side evaluated to 524.383683589 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) Warning: Constraint [v_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [V]... >= Kv_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8881183852 volt but the right hand side evaluated to 34.854287508 volt (Allowable error: 0.0001%, Actual error: 0.097%) Warning: Constraint [i_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [A]... >= 9.55*i0_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.8052896694 ampere but the right hand side evaluated to 522.898341882 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) Warning: Constraint [v_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [V]... >= Kv_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9147291699 volt but the right hand side evaluated to 34.8829190091 volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [i_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [A]... >= 9.55*i0_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.816559688 ampere but the right hand side evaluated to 523.00332036 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) Warning: Constraint [v_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [V]... >= Kv_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9117732803 volt but the right hand side evaluated to 34.8797867438 volt (Allowable error: 0.0001%, Actual error: 0.092%) Warning: Constraint [i_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [A]... >= 9.55*i0_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.6413278702 ampere but the right hand side evaluated to 521.363260757 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.081%) Warning: Constraint [v_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [V]... >= Kv_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9429750621 volt but the right hand side evaluated to 34.9132050388 volt (Allowable error: 0.0001%, Actual error: 0.085%) Warning: Constraint [i_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [A]... >= 9.55*i0_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.6629659499 ampere but the right hand side evaluated to 521.565659532 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.082%) Warning: Constraint [v_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [V]... >= Kv_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9386875469 volt but the right hand side evaluated to 34.9086347883 volt (Allowable error: 0.0001%, Actual error: 0.086%) Warning: Constraint [i_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [A]... >= 9.55*i0_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.4724435812 ampere but the right hand side evaluated to 519.781464473 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) Warning: Constraint [v_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [V]... >= Kv_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9736241873 volt but the right hand side evaluated to 34.9459257255 volt (Allowable error: 0.0001%, Actual error: 0.079%) Warning: Constraint [i_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [A]... >= 9.55*i0_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.5066240678 ampere but the right hand side evaluated to 520.101294271 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%) Warning: Constraint [v_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [V]... >= Kv_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.966463834 volt but the right hand side evaluated to 34.9383236899 volt (Allowable error: 0.0001%, Actual error: 0.081%) Warning: Constraint [i_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [A]... >= 9.55*i0_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.2985169574 ampere but the right hand side evaluated to 518.151644212 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.07%) Warning: Constraint [v_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [V]... >= Kv_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0067189581 volt but the right hand side evaluated to 34.9811130525 volt (Allowable error: 0.0001%, Actual error: 0.073%) Warning: Constraint [i_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [A]... >= 9.55*i0_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.3450909539 ampere but the right hand side evaluated to 518.587769239 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.071%) Warning: Constraint [v_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [V]... >= Kv_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9967693296 volt but the right hand side evaluated to 34.9705804291 volt (Allowable error: 0.0001%, Actual error: 0.075%) Warning: Constraint [i_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [A]... >= 9.55*i0_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.1187439346 ampere but the right hand side evaluated to 516.466197105 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%) Warning: Constraint [v_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [V]... >= Kv_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0427792734 volt but the right hand side evaluated to 35.0192928503 volt (Allowable error: 0.0001%, Actual error: 0.067%) Warning: Constraint [i_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [A]... >= 9.55*i0_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.1771811463 ampere but the right hand side evaluated to 517.013988556 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [v_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [V]... >= Kv_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.030391961 volt but the right hand side evaluated to 35.0062092435 volt (Allowable error: 0.0001%, Actual error: 0.069%) Warning: Constraint [i_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [A]... >= 9.55*i0_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.9316086855 ampere but the right hand side evaluated to 514.710899228 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.058%) Warning: Constraint [v_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [V]... >= Kv_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0828222725 volt but the right hand side evaluated to 35.0615005718 volt (Allowable error: 0.0001%, Actual error: 0.061%) Warning: Constraint [i_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [A]... >= 9.55*i0_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.0036059342 ampere but the right hand side evaluated to 515.38621133 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.06%) Warning: Constraint [v_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [V]... >= Kv_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0667942944 volt but the right hand side evaluated to 35.04463711 volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [i_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [A]... >= 9.55*i0_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.7362527867 ampere but the right hand side evaluated to 512.877461401 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%) Warning: Constraint [v_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [V]... >= Kv_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1274066463 volt but the right hand side evaluated to 35.10828989 volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [i_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [A]... >= 9.55*i0_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.8228235162 ampere but the right hand side evaluated to 513.689978371 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%) Warning: Constraint [v_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [V]... >= Kv_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1070127763 volt but the right hand side evaluated to 35.0869195913 volt (Allowable error: 0.0001%, Actual error: 0.057%) Warning: Constraint [i_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [A]... >= 9.55*i0_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.532219567 ampere but the right hand side evaluated to 510.961231573 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.046%) Warning: Constraint [v_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [V]... >= Kv_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1768117273 volt but the right hand side evaluated to 35.1599212025 volt (Allowable error: 0.0001%, Actual error: 0.048%) Warning: Constraint [i_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [A]... >= 9.55*i0_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.634354612 ampere but the right hand side evaluated to 511.920520356 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.049%) Warning: Constraint [v_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [V]... >= Kv_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1513420357 volt but the right hand side evaluated to 35.1333390899 volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [i_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [A]... >= 9.55*i0_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.3163571437 ampere but the right hand side evaluated to 508.932498818 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.04%) Warning: Constraint [v_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [V]... >= Kv_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.2332039388 volt but the right hand side evaluated to 35.2185895945 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [A]... >= 9.55*i0_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.4360592233 ampere but the right hand side evaluated to 510.057634296 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.043%) Warning: Constraint [v_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [V]... >= Kv_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.2012388214 volt but the right hand side evaluated to 35.1853698712 volt (Allowable error: 0.0001%, Actual error: 0.045%) Warning: Constraint [i_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [A]... >= 9.55*i0_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.0863025383 ampere but the right hand side evaluated to 506.768565338 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.033%) Warning: Constraint [v_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [V]... >= Kv_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.2982048172 volt but the right hand side evaluated to 35.2859093893 volt (Allowable error: 0.0001%, Actual error: 0.035%) Warning: Constraint [i_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [A]... >= 9.55*i0_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.2260967134 ampere but the right hand side evaluated to 508.083694084 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.037%) Warning: Constraint [v_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [V]... >= Kv_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.2579542723 volt but the right hand side evaluated to 35.2442613128 volt (Allowable error: 0.0001%, Actual error: 0.039%) Warning: Constraint [i_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [A]... >= 9.55*i0_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.8379355616 ampere but the right hand side evaluated to 504.430054534 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [v_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [V]... >= Kv_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.3746773777 volt but the right hand side evaluated to 35.3647439191 volt (Allowable error: 0.0001%, Actual error: 0.028%) Warning: Constraint [i_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [A]... >= 9.55*i0_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.0016016191 ampere but the right hand side evaluated to 505.97133179 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.031%) Warning: Constraint [v_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [V]... >= Kv_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.3234627718 volt but the right hand side evaluated to 35.3119894908 volt (Allowable error: 0.0001%, Actual error: 0.032%) Warning: Constraint [i_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [A]... >= 9.55*i0_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.564032201 ampere but the right hand side evaluated to 501.847996519 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.02%) Warning: Constraint [v_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [V]... >= Kv_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.4676825952 volt but the right hand side evaluated to 35.4601585919 volt (Allowable error: 0.0001%, Actual error: 0.021%) Warning: Constraint [i_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [A]... >= 9.55*i0_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.7585501128 ampere but the right hand side evaluated to 503.682031098 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.025%) Warning: Constraint [v_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [V]... >= Kv_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.4005617939 volt but the right hand side evaluated to 35.3913478568 volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [i_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [A]... >= 9.55*i0_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.2511821384 ampere but the right hand side evaluated to 498.894235364 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [V]... >= Kv_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.5866744317 volt but the right hand side evaluated to 35.5816052342 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [A]... >= 9.55*i0_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.4893884266 ampere but the right hand side evaluated to 501.143678332 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.019%) Warning: Constraint [v_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [V]... >= Kv_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.4945466421 volt but the right hand side evaluated to 35.4876363872 volt (Allowable error: 0.0001%, Actual error: 0.019%) Warning: Constraint [i_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [A]... >= 9.55*i0_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.864008574 ampere but the right hand side evaluated to 495.230893642 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0068%) Warning: Constraint [v_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [V]... >= Kv_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.756696682 volt but the right hand side evaluated to 35.7541317514 volt (Allowable error: 0.0001%, Actual error: 0.0072%) Warning: Constraint [i_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [A]... >= 9.55*i0_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.1787663738 ampere but the right hand side evaluated to 498.209734378 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [V]... >= Kv_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.6162404206 volt but the right hand side evaluated to 35.6116863064 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1991 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0328 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0367 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1991 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0328 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0367 but bound is 0.0500 Using solver 'mosek' Solving for 9073 variables. Solving took 2.33 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2351 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 988744.2525 but bound is 600000.0000 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2106 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0340 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0369 but bound is 0.0500 Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 99.8053586052 ampere but the right hand side evaluated to 936.51348806 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 99.7125367663 ampere but the right hand side evaluated to 936.513488067 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 99.58659483 ampere but the right hand side evaluated to 936.513488073 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 99.3939660149 ampere but the right hand side evaluated to 936.513488078 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 99.0931269921 ampere but the right hand side evaluated to 936.513488086 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 38.2500451461 volt but the right hand side evaluated to 37.514077418 volt (Allowable error: 0.0001%, Actual error: 2%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 38.1813116705 volt but the right hand side evaluated to 37.4858738262 volt (Allowable error: 0.0001%, Actual error: 1.9%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 38.0772346671 volt but the right hand side evaluated to 37.4367677623 volt (Allowable error: 0.0001%, Actual error: 1.7%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 37.9163404395 volt but the right hand side evaluated to 37.3595017064 volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 37.6635835592 volt but the right hand side evaluated to 37.236168113 volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [A]... >= 9.55*i0_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.8561545855 ampere but the right hand side evaluated to 627.637728664 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [V]... >= Kv_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0193479074 volt but the right hand side evaluated to 34.9458879015 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [A]... >= 9.55*i0_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.8479245227 ampere but the right hand side evaluated to 627.55804574 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [V]... >= Kv_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0179742277 volt but the right hand side evaluated to 34.9444437978 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [A]... >= 9.55*i0_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.5671103297 ampere but the right hand side evaluated to 624.94478338 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [V]... >= Kv_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0397531146 volt but the right hand side evaluated to 34.9699437838 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [A]... >= 9.55*i0_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.5694993281 ampere but the right hand side evaluated to 624.962357637 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [V]... >= Kv_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0364693114 volt but the right hand side evaluated to 34.9663573016 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [A]... >= 9.55*i0_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.2730564321 ampere but the right hand side evaluated to 622.206544822 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [V]... >= Kv_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0631698298 volt but the right hand side evaluated to 34.9971872585 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [A]... >= 9.55*i0_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.2858690646 ampere but the right hand side evaluated to 622.319966121 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [V]... >= Kv_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0580635521 volt but the right hand side evaluated to 34.9915691974 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [A]... >= 9.55*i0_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.980217605 ampere but the right hand side evaluated to 619.475345316 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [V]... >= Kv_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0853612099 volt but the right hand side evaluated to 35.0229720429 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [A]... >= 9.55*i0_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 65.0009079145 ampere but the right hand side evaluated to 619.663174678 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [V]... >= Kv_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.0800810621 volt but the right hand side evaluated to 35.0171348425 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [A]... >= 9.55*i0_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.6876961006 ampere but the right hand side evaluated to 616.743694158 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [V]... >= Kv_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1068507704 volt but the right hand side evaluated to 35.0478813325 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [A]... >= 9.55*i0_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.7128085329 ampere but the right hand side evaluated to 616.976443309 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [V]... >= Kv_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1036426135 volt but the right hand side evaluated to 35.0442745604 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [A]... >= 9.55*i0_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.3850761773 ampere but the right hand side evaluated to 613.922242991 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [V]... >= Kv_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1344529949 volt but the right hand side evaluated to 35.0793209603 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [A]... >= 9.55*i0_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.4225136923 ampere but the right hand side evaluated to 614.26751842 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [V]... >= Kv_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1280342117 volt but the right hand side evaluated to 35.0722015489 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [A]... >= 9.55*i0_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.0817609864 ampere but the right hand side evaluated to 611.090951922 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [V]... >= Kv_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.161841671 volt but the right hand side evaluated to 35.1103917567 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [A]... >= 9.55*i0_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 64.126298255 ampere but the right hand side evaluated to 611.504116748 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [V]... >= Kv_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1556356207 volt but the right hand side evaluated to 35.1034894654 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [A]... >= 9.55*i0_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 63.7761924212 ampere but the right hand side evaluated to 608.23632914 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [V]... >= Kv_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1899652107 volt but the right hand side evaluated to 35.14212233 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [A]... >= 9.55*i0_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 63.826665936 ampere but the right hand side evaluated to 608.707304869 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [V]... >= Kv_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.1846991226 volt but the right hand side evaluated to 35.1362251004 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [A]... >= 9.55*i0_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 63.4628593642 ampere but the right hand side evaluated to 605.310236342 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [V]... >= Kv_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 35.222366041 volt but the right hand side evaluated to 35.1783229833 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [A]... >= 9.55*i0_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 63.5245047317 ampere but the right hand side evaluated to 605.884516658 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [V]... >= Kv_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 35.2145539565 volt but the right hand side evaluated to 35.169675567 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [A]... >= 9.55*i0_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 63.1453597894 ampere but the right hand side evaluated to 602.343352273 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [V]... >= Kv_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 35.2565788154 volt but the right hand side evaluated to 35.2163113039 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [A]... >= 9.55*i0_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 63.2146462713 ampere but the right hand side evaluated to 602.990438731 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [V]... >= Kv_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 35.2485157316 volt but the right hand side evaluated to 35.2073988513 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [A]... >= 9.55*i0_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.8220491144 ampere but the right hand side evaluated to 599.32088471 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) Warning: Constraint [v_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [V]... >= Kv_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.2935930844 volt but the right hand side evaluated to 35.2571326347 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [A]... >= 9.55*i0_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.901123139 ampere but the right hand side evaluated to 600.059712172 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [V]... >= Kv_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.2838390549 volt but the right hand side evaluated to 35.2464194714 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [A]... >= 9.55*i0_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.4925583136 ampere but the right hand side evaluated to 596.239061427 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) Warning: Constraint [v_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [V]... >= Kv_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.3335572874 volt but the right hand side evaluated to 35.3009219843 volt (Allowable error: 0.0001%, Actual error: 0.092%) Warning: Constraint [i_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [A]... >= 9.55*i0_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.5796605958 ampere but the right hand side evaluated to 597.054395617 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.09%) Warning: Constraint [v_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [V]... >= Kv_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.3232404717 volt but the right hand side evaluated to 35.2896293302 volt (Allowable error: 0.0001%, Actual error: 0.095%) Warning: Constraint [i_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [A]... >= 9.55*i0_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.1578830637 ampere but the right hand side evaluated to 593.10617881 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%) Warning: Constraint [v_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [V]... >= Kv_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.3757264517 volt but the right hand side evaluated to 35.3468613373 volt (Allowable error: 0.0001%, Actual error: 0.082%) Warning: Constraint [i_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [A]... >= 9.55*i0_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.2516837251 ampere but the right hand side evaluated to 593.986372493 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [v_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [V]... >= Kv_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.365690615 volt but the right hand side evaluated to 35.3358966008 volt (Allowable error: 0.0001%, Actual error: 0.084%) Warning: Constraint [i_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [A]... >= 9.55*i0_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.806771782 ampere but the right hand side evaluated to 589.821588701 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [v_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [V]... >= Kv_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.4273658688 volt but the right hand side evaluated to 35.4026385437 volt (Allowable error: 0.0001%, Actual error: 0.07%) Warning: Constraint [i_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [A]... >= 9.55*i0_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.9157105134 ampere but the right hand side evaluated to 590.841908963 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.069%) Warning: Constraint [v_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [V]... >= Kv_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.4120668701 volt but the right hand side evaluated to 35.3861261917 volt (Allowable error: 0.0001%, Actual error: 0.073%) Warning: Constraint [i_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [A]... >= 9.55*i0_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.4495280187 ampere but the right hand side evaluated to 586.475748545 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%) Warning: Constraint [v_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [V]... >= Kv_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.4816325148 volt but the right hand side evaluated to 35.4609243975 volt (Allowable error: 0.0001%, Actual error: 0.058%) Warning: Constraint [i_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [A]... >= 9.55*i0_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.5712376618 ampere but the right hand side evaluated to 587.615797903 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.059%) Warning: Constraint [v_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [V]... >= Kv_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.4626035545 volt but the right hand side evaluated to 35.4405298701 volt (Allowable error: 0.0001%, Actual error: 0.062%) Warning: Constraint [i_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [A]... >= 9.55*i0_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.0866817702 ampere but the right hand side evaluated to 583.072988575 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.045%) Warning: Constraint [v_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [V]... >= Kv_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.5380930857 volt but the right hand side evaluated to 35.5212382847 volt (Allowable error: 0.0001%, Actual error: 0.047%) Warning: Constraint [i_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [A]... >= 9.55*i0_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 61.2164194433 ampere but the right hand side evaluated to 584.290705504 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.048%) Warning: Constraint [v_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [V]... >= Kv_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.5184103521 volt but the right hand side evaluated to 35.5002380338 volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [i_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [A]... >= 9.55*i0_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 60.700552085 ampere but the right hand side evaluated to 579.452985745 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.034%) Warning: Constraint [v_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [V]... >= Kv_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.608176318 volt but the right hand side evaluated to 35.5955518035 volt (Allowable error: 0.0001%, Actual error: 0.035%) Warning: Constraint [i_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [A]... >= 9.55*i0_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 60.8482167522 ampere but the right hand side evaluated to 580.838213566 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [V]... >= Kv_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.5813704419 volt but the right hand side evaluated to 35.5671756923 volt (Allowable error: 0.0001%, Actual error: 0.04%) Warning: Constraint [i_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [A]... >= 9.55*i0_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 60.300708967 ampere but the right hand side evaluated to 575.699965461 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.022%) Warning: Constraint [v_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [V]... >= Kv_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.6855327794 volt but the right hand side evaluated to 35.6770679251 volt (Allowable error: 0.0001%, Actual error: 0.024%) Warning: Constraint [i_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [A]... >= 9.55*i0_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 60.4639007707 ampere but the right hand side evaluated to 577.232164565 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [v_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [V]... >= Kv_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.6531577824 volt but the right hand side evaluated to 35.6430158767 volt (Allowable error: 0.0001%, Actual error: 0.028%) Warning: Constraint [i_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [A]... >= 9.55*i0_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8791591274 ampere but the right hand side evaluated to 571.739248605 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [V]... >= Kv_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.7752524698 volt but the right hand side evaluated to 35.7709876352 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [A]... >= 9.55*i0_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 60.0608422653 ampere but the right hand side evaluated to 573.446746715 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.016%) Warning: Constraint [v_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [V]... >= Kv_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.7353737506 volt but the right hand side evaluated to 35.7293207916 volt (Allowable error: 0.0001%, Actual error: 0.017%) Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2106 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0340 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0369 but bound is 0.0500 Warning: Constraint [i_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [A]... >= 9.55*i0_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6316150477 ampere but the right hand side evaluated to 569.411419133 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.005%) Warning: Constraint [v_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [V]... >= Kv_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.83271024 volt but the right hand side evaluated to 35.8308144951 volt (Allowable error: 0.0001%, Actual error: 0.0053%) Using solver 'mosek' Solving for 4713 variables. Solving took 1.01 seconds. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.2058 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1064456.8431 but bound is 600000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 111.917770052 ampere but the right hand side evaluated to 1056.06638259 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 111.846508662 ampere but the right hand side evaluated to 1056.0663826 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 111.750496698 ampere but the right hand side evaluated to 1056.06638261 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 111.604583491 ampere but the right hand side evaluated to 1056.06638263 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 111.378520141 ampere but the right hand side evaluated to 1056.06638264 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 38.2100050587 volt but the right hand side evaluated to 37.703700589 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 38.1552266825 volt but the right hand side evaluated to 37.676874408 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 38.0707683706 volt but the right hand side evaluated to 37.6300619441 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 37.9401395681 volt but the right hand side evaluated to 37.5563494017 volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 37.7350514783 volt but the right hand side evaluated to 37.438674283 volt (Allowable error: 0.0001%, Actual error: 0.79%) Warning: Constraint [i_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [A]... >= 9.55*i0_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 73.3928809075 ampere but the right hand side evaluated to 699.259437341 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [V]... >= Kv_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.2475796756 volt but the right hand side evaluated to 35.1620021793 volt (Allowable error: 0.0001%, Actual error: 0.24%) Warning: Constraint [i_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [A]... >= 9.55*i0_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 73.0287800896 ampere but the right hand side evaluated to 695.874661344 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [V]... >= Kv_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.2657860571 volt but the right hand side evaluated to 35.1847556766 volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [i_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [A]... >= 9.55*i0_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 72.6668707247 ampere but the right hand side evaluated to 692.503909994 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [V]... >= Kv_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.2825360344 volt but the right hand side evaluated to 35.2057286888 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [A]... >= 9.55*i0_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 72.3030178084 ampere but the right hand side evaluated to 689.114223932 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [V]... >= Kv_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.3004423704 volt but the right hand side evaluated to 35.2278760326 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [A]... >= 9.55*i0_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 71.9368569251 ampere but the right hand side evaluated to 685.702214533 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [V]... >= Kv_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.319619583 volt but the right hand side evaluated to 35.2513177671 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [A]... >= 9.55*i0_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 71.5698251276 ampere but the right hand side evaluated to 682.279116183 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [V]... >= Kv_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.339012059 volt but the right hand side evaluated to 35.2748651266 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [A]... >= 9.55*i0_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 71.1962375207 ampere but the right hand side evaluated to 678.798172587 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [V]... >= Kv_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.3621860732 volt but the right hand side evaluated to 35.3024907896 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [A]... >= 9.55*i0_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 70.8211296589 ampere but the right hand side evaluated to 675.299841866 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [V]... >= Kv_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.3857488327 volt but the right hand side evaluated to 35.3303922636 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [A]... >= 9.55*i0_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 70.4425563445 ampere but the right hand side evaluated to 671.767772507 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [V]... >= Kv_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.4108388785 volt but the right hand side evaluated to 35.3598286042 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [A]... >= 9.55*i0_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 70.0657091443 ampere but the right hand side evaluated to 668.244857313 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [V]... >= Kv_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.4340101959 volt but the right hand side evaluated to 35.3869854277 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [A]... >= 9.55*i0_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 69.6718387141 ampere but the right hand side evaluated to 664.57383587 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [V]... >= Kv_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.4671381102 volt but the right hand side evaluated to 35.4249433772 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [A]... >= 9.55*i0_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 69.2796432549 ampere but the right hand side evaluated to 660.910358539 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [V]... >= Kv_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.498126478 volt but the right hand side evaluated to 35.4603417137 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [A]... >= 9.55*i0_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 68.8779735265 ampere but the right hand side evaluated to 657.159927166 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%) Warning: Constraint [v_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [V]... >= Kv_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.533956436 volt but the right hand side evaluated to 35.5008295264 volt (Allowable error: 0.0001%, Actual error: 0.093%) Warning: Constraint [i_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [A]... >= 9.55*i0_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 68.4704569338 ampere but the right hand side evaluated to 653.352346267 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) Warning: Constraint [v_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [V]... >= Kv_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.5721823924 volt but the right hand side evaluated to 35.5436931336 volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [i_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [A]... >= 9.55*i0_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 68.056541243 ampere but the right hand side evaluated to 649.482187165 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [v_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [V]... >= Kv_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.6130215752 volt but the right hand side evaluated to 35.5891420148 volt (Allowable error: 0.0001%, Actual error: 0.067%) Warning: Constraint [i_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [A]... >= 9.55*i0_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 67.634264213 ampere but the right hand side evaluated to 645.531677118 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [V]... >= Kv_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.6575716444 volt but the right hand side evaluated to 35.6383309899 volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [i_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [A]... >= 9.55*i0_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 67.2007894609 ampere but the right hand side evaluated to 641.474965924 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [V]... >= Kv_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.7074599538 volt but the right hand side evaluated to 35.6929628154 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [A]... >= 9.55*i0_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 66.7560033352 ampere but the right hand side evaluated to 637.30952997 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [V]... >= Kv_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.7625903813 volt but the right hand side evaluated to 35.7528622718 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [A]... >= 9.55*i0_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 66.2964767541 ampere but the right hand side evaluated to 633.003334149 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [V]... >= Kv_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.8249158544 volt but the right hand side evaluated to 35.8200292515 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 571 variables. Solving took 0.199 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2058 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1064456.8406 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 111.920982833 ampere but the right hand side evaluated to 1056.0663751 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 111.849323672 ampere but the right hand side evaluated to 1056.06637512 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 111.752850386 ampere but the right hand side evaluated to 1056.06637514 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 111.606364764 ampere but the right hand side evaluated to 1056.06637516 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 111.379914674 ampere but the right hand side evaluated to 1056.06637518 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 38.2086428026 volt but the right hand side evaluated to 37.7038065545 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 38.1536792396 volt but the right hand side evaluated to 37.6769672477 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 38.0690626248 volt but the right hand side evaluated to 37.6301395605 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 37.9383538985 volt but the right hand side evaluated to 37.5564081288 volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 37.7337082178 volt but the right hand side evaluated to 37.4387202459 volt (Allowable error: 0.0001%, Actual error: 0.79%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 571 variables. Solving took 0.164 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2058 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1064456.8406 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 111.920983071 ampere but the right hand side evaluated to 1056.06637509 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 111.849323864 ampere but the right hand side evaluated to 1056.06637511 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 111.752850524 ampere but the right hand side evaluated to 1056.06637513 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 111.606364832 ampere but the right hand side evaluated to 1056.06637515 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 111.379914696 ampere but the right hand side evaluated to 1056.06637517 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 38.208642739 volt but the right hand side evaluated to 37.7038065622 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 38.1536791587 volt but the right hand side evaluated to 37.6769672538 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 38.0690625246 volt but the right hand side evaluated to 37.6301395648 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 37.9383537792 volt but the right hand side evaluated to 37.5564081308 volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 37.7337081204 volt but the right hand side evaluated to 37.4387202465 volt (Allowable error: 0.0001%, Actual error: 0.79%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 4713 variables. Solving took 1.16 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2058 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1064456.8435 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 111.91781048 ampere but the right hand side evaluated to 1056.06638257 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 111.846541075 ampere but the right hand side evaluated to 1056.06638258 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 111.750518933 ampere but the right hand side evaluated to 1056.0663826 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 111.604592233 ampere but the right hand side evaluated to 1056.06638261 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 111.378511001 ampere but the right hand side evaluated to 1056.06638263 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 38.2100217709 volt but the right hand side evaluated to 37.7037019448 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 38.1552398257 volt but the right hand side evaluated to 37.6768754992 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 38.070777112 volt but the right hand side evaluated to 37.6300626995 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 37.940142573 volt but the right hand side evaluated to 37.5563497118 volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 37.7350478144 volt but the right hand side evaluated to 37.4386740031 volt (Allowable error: 0.0001%, Actual error: 0.79%) Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 73.3931399317 ampere but the right hand side evaluated to 699.262943383 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 35.2475644303 volt but the right hand side evaluated to 35.1620428012 volt (Allowable error: 0.0001%, Actual error: 0.24%) Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 73.0289049949 ampere but the right hand side evaluated to 695.876969183 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.2658444919 volt but the right hand side evaluated to 35.1848744094 volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 72.6669887713 ampere but the right hand side evaluated to 692.506036695 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.2825856688 volt but the right hand side evaluated to 35.2058326465 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 72.3031318237 ampere but the right hand side evaluated to 689.116198282 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.3004819325 volt but the right hand side evaluated to 35.2279639881 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 71.9369637891 ampere but the right hand side evaluated to 685.704017571 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.3196516875 volt but the right hand side evaluated to 35.2513928635 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 71.5699950948 ampere but the right hand side evaluated to 682.281328939 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.3389920492 volt but the right hand side evaluated to 35.274877826 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 71.1963081385 ampere but the right hand side evaluated to 678.799470934 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.3622191785 volt but the right hand side evaluated to 35.3025585123 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 70.8211717363 ampere but the right hand side evaluated to 675.300809206 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.3857899763 volt but the right hand side evaluated to 35.3304649206 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 70.4426759546 ampere but the right hand side evaluated to 671.769293711 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.410820512 volt but the right hand side evaluated to 35.3598315971 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 70.0648746622 ampere but the right hand side evaluated to 668.23833607 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 35.4345945362 volt but the right hand side evaluated to 35.387650194 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 69.6718343987 ampere but the right hand side evaluated to 664.574163311 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.4671815905 volt but the right hand side evaluated to 35.4250077244 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 69.2794508201 ampere but the right hand side evaluated to 660.909022271 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.4982818287 volt but the right hand side evaluated to 35.4605254377 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 68.8780413361 ampere but the right hand side evaluated to 657.160731274 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%) Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.533939118 volt but the right hand side evaluated to 35.500821244 volt (Allowable error: 0.0001%, Actual error: 0.093%) Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 68.4705011768 ampere but the right hand side evaluated to 653.352894171 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.57217367 volt but the right hand side evaluated to 35.5436916813 volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 68.0565747141 ampere but the right hand side evaluated to 649.482595386 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.6130142097 volt but the right hand side evaluated to 35.5891398158 volt (Allowable error: 0.0001%, Actual error: 0.067%) Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 67.6342936614 ampere but the right hand side evaluated to 645.53201139 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.6575622376 volt but the right hand side evaluated to 35.6383246967 volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 67.200804915 ampere but the right hand side evaluated to 641.475147247 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.707455678 volt but the right hand side evaluated to 35.6929605256 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 66.7560125128 ampere but the right hand side evaluated to 637.309632008 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.7625871689 volt but the right hand side evaluated to 35.7528599122 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 66.296478799 ampere but the right hand side evaluated to 633.00335761 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.8249152384 volt but the right hand side evaluated to 35.8200288701 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Beginning signomial solve. Solving took 4 GP solves and 7.42 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), CL_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2115 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 1024485.2866 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2113 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0257 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0393 but bound is 0.0500 Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 103.180116482 ampere but the right hand side evaluated to 968.100177777 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 103.085445972 ampere but the right hand side evaluated to 968.100177795 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 102.957161685 ampere but the right hand side evaluated to 968.100177809 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 102.761207112 ampere but the right hand side evaluated to 968.100177828 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 102.455482094 ampere but the right hand side evaluated to 968.100177853 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 37.9242671602 volt but the right hand side evaluated to 37.1871423443 volt (Allowable error: 0.0001%, Actual error: 2%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 37.8575886955 volt but the right hand side evaluated to 37.1603769096 volt (Allowable error: 0.0001%, Actual error: 1.9%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 37.7565345226 volt but the right hand side evaluated to 37.1133868754 volt (Allowable error: 0.0001%, Actual error: 1.7%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 37.6004436505 volt but the right hand side evaluated to 37.0394318447 volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 37.3554068199 volt but the right hand side evaluated to 36.9213677198 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 68.3453815901 ampere but the right hand side evaluated to 651.14739435 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.6911556149 volt but the right hand side evaluated to 34.6060531533 volt (Allowable error: 0.0001%, Actual error: 0.25%) Warning: Constraint [i_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 67.9970156316 ampere but the right hand side evaluated to 647.9089882 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.7124926171 volt but the right hand side evaluated to 34.6319596916 volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [i_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 67.6517504928 ampere but the right hand side evaluated to 644.692671896 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [v_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.7317735201 volt but the right hand side evaluated to 34.6554359524 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 67.3042186804 ampere but the right hand side evaluated to 641.454324 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.7524589839 volt but the right hand side evaluated to 34.6803337967 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 66.9539902348 ampere but the right hand side evaluated to 638.189956726 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.7747171185 volt but the right hand side evaluated to 34.7068286708 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 66.6031147856 ampere but the right hand side evaluated to 634.916343404 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.7970876937 volt but the right hand side evaluated to 34.7333033322 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 66.2438495214 ampere but the right hand side evaluated to 631.568038086 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8245376922 volt but the right hand side evaluated to 34.7652050761 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 65.8831989404 ampere but the right hand side evaluated to 628.20331953 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8523536382 volt but the right hand side evaluated to 34.7973357593 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 65.5190194381 ampere but the right hand side evaluated to 624.803761817 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8818299401 volt but the right hand side evaluated to 34.8311054462 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 65.1525091144 ampere but the right hand side evaluated to 621.379256307 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9120773269 volt but the right hand side evaluated to 34.8655353718 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 64.7735918552 ampere but the right hand side evaluated to 617.842580976 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9495232735 volt but the right hand side evaluated to 34.9075775205 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 64.3922722059 ampere but the right hand side evaluated to 614.279017306 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9875505985 volt but the right hand side evaluated to 34.9500212955 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 64.0015324089 ampere but the right hand side evaluated to 610.627132897 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.089%) Warning: Constraint [v_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0305878523 volt but the right hand side evaluated to 34.9976240965 volt (Allowable error: 0.0001%, Actual error: 0.094%) Warning: Constraint [i_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 63.6023455472 ampere but the right hand side evaluated to 606.894355658 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) Warning: Constraint [v_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0778803556 volt but the right hand side evaluated to 35.0495250527 volt (Allowable error: 0.0001%, Actual error: 0.081%) Warning: Constraint [i_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 63.1951815953 ampere but the right hand side evaluated to 603.083898309 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%) Warning: Constraint [v_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1290044622 volt but the right hand side evaluated to 35.1052265959 volt (Allowable error: 0.0001%, Actual error: 0.068%) Warning: Constraint [i_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 62.7772999441 ampere but the right hand side evaluated to 599.170553889 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1856009352 volt but the right hand side evaluated to 35.1664300671 volt (Allowable error: 0.0001%, Actual error: 0.055%) Warning: Constraint [i_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 62.3445853958 ampere but the right hand side evaluated to 595.116277396 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.039%) Warning: Constraint [v_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.2501808617 volt but the right hand side evaluated to 35.2357279606 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [A]... >= 9.55*i0_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.8960720153 ampere but the right hand side evaluated to 590.910400962 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [V]... >= Kv_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.3232153463 volt but the right hand side evaluated to 35.3135091173 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.4259305284 ampere but the right hand side evaluated to 586.497970584 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.4082784509 volt but the right hand side evaluated to 35.4033990865 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2113 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0257 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0393 but bound is 0.0500 Using solver 'mosek_cli' Solving for 4713 variables. Solving took 1.08 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2058 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1064461.9306 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 111.91772465 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 111.84645576 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 111.750532658 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 111.604570119 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 111.378465399 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 38.2099900097 volt but the right hand side evaluated to 37.7037124356 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 38.1552361519 volt but the right hand side evaluated to 37.6768818679 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 38.070777763 volt but the right hand side evaluated to 37.6300725084 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 37.9401531069 volt but the right hand side evaluated to 37.5563550079 volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 37.7350360091 volt but the right hand side evaluated to 37.4386798186 volt (Allowable error: 0.0001%, Actual error: 0.79%) Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 73.3928852703 ampere but the right hand side evaluated to 699.259252504 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 35.2475844264 volt but the right hand side evaluated to 35.1620175348 volt (Allowable error: 0.0001%, Actual error: 0.24%) Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 73.0288084791 ampere but the right hand side evaluated to 695.875002379 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.2657768732 volt but the right hand side evaluated to 35.1847586308 volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 72.6669010809 ampere but the right hand side evaluated to 692.503656937 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.2825320963 volt but the right hand side evaluated to 35.2057381181 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 72.3030273248 ampere but the right hand side evaluated to 689.114181043 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.3004601759 volt but the right hand side evaluated to 35.2278680724 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 71.9368751189 ampere but the right hand side evaluated to 685.702542038 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.3196335309 volt but the right hand side evaluated to 35.2513063048 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 71.5698574506 ampere but the right hand side evaluated to 682.278868389 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.3389939944 volt but the right hand side evaluated to 35.2748531353 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 71.196239428 ampere but the right hand side evaluated to 678.798399874 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.3621839799 volt but the right hand side evaluated to 35.302504444 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 70.8211014944 ampere but the right hand side evaluated to 675.299571033 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.3857430387 volt but the right hand side evaluated to 35.3303851139 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 70.4425863487 ampere but the right hand side evaluated to 671.76780333 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 35.4108404265 volt but the right hand side evaluated to 35.3598222095 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 70.0656738448 ampere but the right hand side evaluated to 668.244506754 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 35.4340066907 volt but the right hand side evaluated to 35.3869840023 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 69.6718247479 ampere but the right hand side evaluated to 664.573718666 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.4671529804 volt but the right hand side evaluated to 35.4249283144 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 69.2796352934 ampere but the right hand side evaluated to 660.910267925 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.4981293242 volt but the right hand side evaluated to 35.4603518177 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 68.8779432657 ampere but the right hand side evaluated to 657.159687095 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%) Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.5339650128 volt but the right hand side evaluated to 35.5008151603 volt (Allowable error: 0.0001%, Actual error: 0.093%) Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 68.4704318325 ampere but the right hand side evaluated to 653.35251579 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.5721845645 volt but the right hand side evaluated to 35.5437029519 volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 68.0565515503 ampere but the right hand side evaluated to 649.482206845 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.6130092687 volt but the right hand side evaluated to 35.5891434405 volt (Allowable error: 0.0001%, Actual error: 0.067%) Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 67.6342830362 ampere but the right hand side evaluated to 645.531584282 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.6575890221 volt but the right hand side evaluated to 35.6383203702 volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 67.2007897707 ampere but the right hand side evaluated to 641.475009679 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.7074731924 volt but the right hand side evaluated to 35.6929701349 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 66.7559879251 ampere but the right hand side evaluated to 637.309625955 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.7625765899 volt but the right hand side evaluated to 35.7528572379 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 66.2964930089 ampere but the right hand side evaluated to 633.003278394 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 35.8249292918 volt but the right hand side evaluated to 35.8200255905 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500 Beginning signomial solve. Solving took 4 GP solves and 9.19 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), CL_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2115 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 1024484.3799 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2113 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0257 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0393 but bound is 0.0500 Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 103.179893125 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 103.085320531 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 102.957059166 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 102.761215428 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 102.455545289 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 37.9241836643 volt but the right hand side evaluated to 37.1871409632 volt (Allowable error: 0.0001%, Actual error: 2%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 37.8575336611 volt but the right hand side evaluated to 37.1603807992 volt (Allowable error: 0.0001%, Actual error: 1.9%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 37.7565133544 volt but the right hand side evaluated to 37.1133694409 volt (Allowable error: 0.0001%, Actual error: 1.7%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 37.6004493078 volt but the right hand side evaluated to 37.0394414661 volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 37.3554568011 volt but the right hand side evaluated to 36.9213822508 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 68.3448354525 ampere but the right hand side evaluated to 651.139634182 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.6911634881 volt but the right hand side evaluated to 34.6059019965 volt (Allowable error: 0.0001%, Actual error: 0.25%) Warning: Constraint [i_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 67.9968241222 ampere but the right hand side evaluated to 647.904303437 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.7122968411 volt but the right hand side evaluated to 34.6316097356 volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [i_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 67.6515319775 ampere but the right hand side evaluated to 644.688590865 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [v_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.7316022445 volt but the right hand side evaluated to 34.6551154539 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 67.3040221936 ampere but the right hand side evaluated to 641.450471552 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.7523084493 volt but the right hand side evaluated to 34.6800462207 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 66.9538114289 ampere but the right hand side evaluated to 638.186325829 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.7745918201 volt but the right hand side evaluated to 34.7065860277 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 66.6027587926 ampere but the right hand side evaluated to 634.911569203 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.797098261 volt but the right hand side evaluated to 34.7332078372 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 66.2437419982 ampere but the right hand side evaluated to 631.565945243 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.824389883 volt but the right hand side evaluated to 34.7649868307 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 65.8831685544 ampere but the right hand side evaluated to 628.201774725 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8521908372 volt but the right hand side evaluated to 34.7970991815 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 65.5187918522 ampere but the right hand side evaluated to 624.800974192 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.8818277933 volt but the right hand side evaluated to 34.8310402225 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 65.1548014993 ampere but the right hand side evaluated to 621.397955272 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9104775331 volt but the right hand side evaluated to 34.8637502062 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 64.7737222319 ampere but the right hand side evaluated to 617.842352999 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9493545256 volt but the right hand side evaluated to 34.9073593924 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 64.3928756218 ampere but the right hand side evaluated to 614.283468853 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9870852312 volt but the right hand side evaluated to 34.9494971368 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 64.0014026804 ampere but the right hand side evaluated to 610.625693746 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.089%) Warning: Constraint [v_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0306012177 volt but the right hand side evaluated to 34.9976232036 volt (Allowable error: 0.0001%, Actual error: 0.094%) Warning: Constraint [i_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 63.6022597261 ampere but the right hand side evaluated to 606.893206384 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) Warning: Constraint [v_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0778893875 volt but the right hand side evaluated to 35.0494976305 volt (Allowable error: 0.0001%, Actual error: 0.081%) Warning: Constraint [i_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 63.195114756 ampere but the right hand side evaluated to 603.083311633 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%) Warning: Constraint [v_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1289999939 volt but the right hand side evaluated to 35.1051987827 volt (Allowable error: 0.0001%, Actual error: 0.068%) Warning: Constraint [i_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 62.7772659018 ampere but the right hand side evaluated to 599.170103847 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%) Warning: Constraint [v_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.1856032373 volt but the right hand side evaluated to 35.1664497638 volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [i_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 62.3445338826 ampere but the right hand side evaluated to 595.115806014 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.039%) Warning: Constraint [v_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.2501928442 volt but the right hand side evaluated to 35.2357400308 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [A]... >= 9.55*i0_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.8960893007 ampere but the right hand side evaluated to 590.910211685 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [V]... >= Kv_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.3232009941 volt but the right hand side evaluated to 35.3135051811 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.4259263938 ampere but the right hand side evaluated to 586.497990346 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.4082909378 volt but the right hand side evaluated to 35.4033923764 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2113 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0257 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0393 but bound is 0.0500
Standard Error
/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun)