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Console Output

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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 64.7122701244 ampere but the right hand side evaluated to 616.970217226 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 35.103806331 volt but the right hand side evaluated to 35.0443719061 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 64.384044229 ampere but the right hand side evaluated to 613.911967047 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 35.1349668682 volt but the right hand side evaluated to 35.0798074708 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 64.4207409351 ampere but the right hand side evaluated to 614.250871612 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 35.1290362868 volt but the right hand side evaluated to 35.073217455 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 64.0814741076 ampere but the right hand side evaluated to 611.08723186 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 35.1618818632 volt but the right hand side evaluated to 35.1103717719 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 64.1259649419 ampere but the right hand side evaluated to 611.49996763 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 35.1557029631 volt but the right hand side evaluated to 35.103497464 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 63.7758122199 ampere but the right hand side evaluated to 608.231948347 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 35.190085145 volt but the right hand side evaluated to 35.1421957488 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 63.8263185278 ampere but the right hand side evaluated to 608.703182474 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 35.1847942046 volt but the right hand side evaluated to 35.1362704056 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 63.4387854085 ampere but the right hand side evaluated to 605.09973692 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 35.2381080078 volt but the right hand side evaluated to 35.1952246542 volt (Allowable error: 0.0001%, Actual error: 0.12%)

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 63.524267241 ampere but the right hand side evaluated to 605.881489866 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 35.2145942422 volt but the right hand side evaluated to 35.1696688317 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 63.1434933884 ampere but the right hand side evaluated to 602.326251294 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 35.2577111616 volt but the right hand side evaluated to 35.2174858648 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 63.204062182 ampere but the right hand side evaluated to 602.897179492 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 35.2553803962 volt but the right hand side evaluated to 35.21473232 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 62.8214541311 ampere but the right hand side evaluated to 599.314997904 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 35.2939032894 volt but the right hand side evaluated to 35.257429385 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 62.8436253354 ampere but the right hand side evaluated to 599.553989453 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.093%)

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 35.3214904165 volt but the right hand side evaluated to 35.286699917 volt (Allowable error: 0.0001%, Actual error: 0.099%)

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 62.4922965545 ampere but the right hand side evaluated to 596.236213341 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 35.3336631669 volt but the right hand side evaluated to 35.3010057768 volt (Allowable error: 0.0001%, Actual error: 0.093%)

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 62.5793090361 ampere but the right hand side evaluated to 597.050731896 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 35.3234020817 volt but the right hand side evaluated to 35.2897713919 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 62.1579587009 ampere but the right hand side evaluated to 593.106419852 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 35.3756243116 volt but the right hand side evaluated to 35.3467289654 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 62.2513985968 ampere but the right hand side evaluated to 593.98339823 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 35.3658223893 volt but the right hand side evaluated to 35.3360122765 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 61.8063875926 ampere but the right hand side evaluated to 589.817846596 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 35.4275780594 volt but the right hand side evaluated to 35.4028457773 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 61.9153937434 ampere but the right hand side evaluated to 590.838745008 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 35.4122317678 volt but the right hand side evaluated to 35.386282017 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 61.4444751114 ampere but the right hand side evaluated to 586.430265093 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 35.4849040696 volt but the right hand side evaluated to 35.4643694189 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 61.5711064458 ampere but the right hand side evaluated to 587.614368675 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 35.4626579702 volt but the right hand side evaluated to 35.4405729638 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 61.0867203901 ampere but the right hand side evaluated to 583.073180175 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 35.5380490559 volt but the right hand side evaluated to 35.5211828864 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 61.2154054069 ampere but the right hand side evaluated to 584.281418549 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 35.5190506357 volt but the right hand side evaluated to 35.5009031555 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 60.7002335389 ampere but the right hand side evaluated to 579.45001629 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 35.6083736983 volt but the right hand side evaluated to 35.5957537485 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 60.8479563772 ampere but the right hand side evaluated to 580.835753133 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 35.5815271992 volt but the right hand side evaluated to 35.5673340056 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 60.3004563878 ampere but the right hand side evaluated to 575.697627285 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 35.6856929998 volt but the right hand side evaluated to 35.6772328997 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 60.4545288513 ampere but the right hand side evaluated to 577.147001866 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%)

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 35.659250379 volt but the right hand side evaluated to 35.6493878458 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 59.8771694194 ampere but the right hand side evaluated to 571.721021079 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 35.7765444319 volt but the right hand side evaluated to 35.7723303329 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 60.0604750433 ampere but the right hand side evaluated to 573.443373171 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 35.7356108521 volt but the right hand side evaluated to 35.7295665745 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 59.6315834195 ampere but the right hand side evaluated to 569.411127136 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 35.8327316572 volt but the right hand side evaluated to 35.8308365758 volt (Allowable error: 0.0001%, Actual error: 0.0053%)

Using solver 'mosek'
Solving for 4713 variables.
Solving took 17.6 seconds.
Allowing negative dual variable(s) as small as -2.6156435237073434e-11.
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 111.917788829 ampere but the right hand side evaluated to 1056.06638206 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 111.846523084 ampere but the right hand side evaluated to 1056.06638207 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 111.750505838 ampere but the right hand side evaluated to 1056.06638208 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 111.604585859 ampere but the right hand side evaluated to 1056.0663821 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 111.378514997 ampere but the right hand side evaluated to 1056.06638212 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 38.2100131001 volt but the right hand side evaluated to 37.7037012057 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 38.1552328995 volt but the right hand side evaluated to 37.6768748809 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 38.0707723653 volt but the right hand side evaluated to 37.6300622427 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 37.9401407252 volt but the right hand side evaluated to 37.5563494767 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 37.7350495154 volt but the right hand side evaluated to 37.4386741102 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 73.3929423536 ampere but the right hand side evaluated to 699.26053656 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 35.2476044505 volt but the right hand side evaluated to 35.1620544874 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 73.0288011096 ampere but the right hand side evaluated to 695.875381472 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 35.2658312776 volt but the right hand side evaluated to 35.1848288598 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 72.6669132329 ampere but the right hand side evaluated to 692.504741922 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 35.282560975 volt but the right hand side evaluated to 35.2057767381 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 72.3030642262 ampere but the right hand side evaluated to 689.115035075 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 35.3004592434 volt but the right hand side evaluated to 35.2279129843 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 71.9368512819 ampere but the right hand side evaluated to 685.702563833 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 35.3196660137 volt but the right hand side evaluated to 35.2513862051 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 71.5698161698 ampere but the right hand side evaluated to 682.279393299 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 35.3390559594 volt but the right hand side evaluated to 35.27492892 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 71.1962570558 ampere but the right hand side evaluated to 678.798634934 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 35.3622065058 volt but the right hand side evaluated to 35.3025264754 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 70.8211476796 ampere but the right hand side evaluated to 675.300249459 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 35.3857656947 volt but the right hand side evaluated to 35.3304222284 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 70.4426113503 ampere but the right hand side evaluated to 671.768449182 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 35.4108278748 volt but the right hand side evaluated to 35.3598261255 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 70.0653247141 ampere but the right hand side evaluated to 668.241835647 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 35.4342774251 volt but the right hand side evaluated to 35.387288704 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 69.6718413793 ampere but the right hand side evaluated to 664.574009749 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 35.4671533445 volt but the right hand side evaluated to 35.4249670058 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 69.2795617819 ampere but the right hand side evaluated to 660.909791957 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 35.4981921333 volt but the right hand side evaluated to 35.4604193209 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 68.8780041062 ampere but the right hand side evaluated to 657.160283019 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 35.5339478346 volt but the right hand side evaluated to 35.5008246007 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 68.4704769135 ampere but the right hand side evaluated to 653.352588677 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 35.5721778562 volt but the right hand side evaluated to 35.5436915831 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 68.0565571127 ampere but the right hand side evaluated to 649.482374509 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 35.6130173436 volt but the right hand side evaluated to 35.5891398665 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 67.6342773499 ampere but the right hand side evaluated to 645.531823981 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 35.6575671599 volt but the right hand side evaluated to 35.6383277577 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 67.2007973304 ampere but the right hand side evaluated to 641.475055252 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 35.7074573977 volt but the right hand side evaluated to 35.6929610869 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 66.7558909496 ampere but the right hand side evaluated to 637.308548873 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 35.7626615287 volt but the right hand side evaluated to 35.7529388643 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 66.2964729592 ampere but the right hand side evaluated to 633.003302663 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 35.8249184555 volt but the right hand side evaluated to 35.8200321355 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 13.6 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 1064456.8413 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 111.917805006 ampere but the right hand side evaluated to 1056.06638047 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 111.846524309 ampere but the right hand side evaluated to 1056.06638051 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 111.75048439 ampere but the right hand side evaluated to 1056.06638054 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 111.604534852 ampere but the right hand side evaluated to 1056.06638058 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 111.378430609 ampere but the right hand side evaluated to 1056.06638063 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 38.2100973156 volt but the right hand side evaluated to 37.7037017069 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 38.1553060486 volt but the right hand side evaluated to 37.6768748902 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 38.0708295856 volt but the right hand side evaluated to 37.6300615051 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 37.9401761724 volt but the right hand side evaluated to 37.5563477654 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 37.7350571651 volt but the right hand side evaluated to 37.4386712962 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 8.37 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 1064456.8413 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 111.917804447 ampere but the right hand side evaluated to 1056.06638036 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 111.846523827 ampere but the right hand side evaluated to 1056.0663804 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 111.750483979 ampere but the right hand side evaluated to 1056.06638042 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 111.604534528 ampere but the right hand side evaluated to 1056.06638047 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 111.378430368 ampere but the right hand side evaluated to 1056.06638052 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 38.2100974254 volt but the right hand side evaluated to 37.7037016882 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 38.1553061712 volt but the right hand side evaluated to 37.676874874 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 38.0708297108 volt but the right hand side evaluated to 37.6300614913 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 37.9401762931 volt but the right hand side evaluated to 37.5563477545 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 37.7350572589 volt but the right hand side evaluated to 37.4386712879 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 29.6 seconds.
Allowing negative dual variable(s) as small as -2.4537266361270126e-11.
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 1064456.8436 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 111.917791143 ampere but the right hand side evaluated to 1056.06638228 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 111.846524881 ampere but the right hand side evaluated to 1056.06638229 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 111.750507005 ampere but the right hand side evaluated to 1056.0663823 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 111.604586217 ampere but the right hand side evaluated to 1056.06638232 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 111.378514458 ampere but the right hand side evaluated to 1056.06638233 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 38.2100140726 volt but the right hand side evaluated to 37.7037012828 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 38.1552336507 volt but the right hand side evaluated to 37.676874941 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 38.070772848 volt but the right hand side evaluated to 37.630062282 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 37.9401408656 volt but the right hand side evaluated to 37.5563494894 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 37.7350492819 volt but the right hand side evaluated to 37.4386740933 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 73.3926902076 ampere but the right hand side evaluated to 699.258621717 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 35.2477783541 volt but the right hand side evaluated to 35.1622543064 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 73.028804328 ampere but the right hand side evaluated to 695.875476457 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 35.2658365873 volt but the right hand side evaluated to 35.1848376415 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 72.6669132984 ampere but the right hand side evaluated to 692.504806434 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 35.2825678086 volt but the right hand side evaluated to 35.2057870302 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 72.3030613878 ampere but the right hand side evaluated to 689.11506885 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 35.3004672073 volt but the right hand side evaluated to 35.2279242574 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 71.9368507929 ampere but the right hand side evaluated to 685.702610404 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 35.3196718169 volt but the right hand side evaluated to 35.251394811 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 71.5698626233 ampere but the right hand side evaluated to 682.279813967 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 35.3390304581 volt but the right hand side evaluated to 35.2749022393 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 71.1962558318 ampere but the right hand side evaluated to 678.798663445 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 35.3622115257 volt but the right hand side evaluated to 35.3025337175 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 70.821147693 ampere but the right hand side evaluated to 675.300282493 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 35.3857693182 volt but the right hand side evaluated to 35.3304276836 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 70.4426114256 ampere but the right hand side evaluated to 671.768478198 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 35.4108309775 volt but the right hand side evaluated to 35.3598308115 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 70.0653033159 ampere but the right hand side evaluated to 668.241682603 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 35.4342939975 volt but the right hand side evaluated to 35.387308132 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 69.6718397306 ampere but the right hand side evaluated to 664.574015162 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 35.4671565625 volt but the right hand side evaluated to 35.4249714208 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 69.2795553456 ampere but the right hand side evaluated to 660.909753326 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 35.4981980198 volt but the right hand side evaluated to 35.4604265016 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 68.8780049318 ampere but the right hand side evaluated to 657.160301941 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 35.5339486659 volt but the right hand side evaluated to 35.5008260666 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 68.4704776075 ampere but the right hand side evaluated to 653.352603441 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 35.5721784303 volt but the right hand side evaluated to 35.5436926282 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 68.0565577422 ampere but the right hand side evaluated to 649.482386172 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 35.61301767 volt but the right hand side evaluated to 35.5891405225 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 67.6342784916 ampere but the right hand side evaluated to 645.531837911 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 35.657566914 volt but the right hand side evaluated to 35.6383276902 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 67.2007974696 ampere but the right hand side evaluated to 641.475058778 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 35.7074575869 volt but the right hand side evaluated to 35.692961406 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 66.7560006506 ampere but the right hand side evaluated to 637.309516242 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 35.7625932107 volt but the right hand side evaluated to 35.7528658048 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 66.2964785401 ampere but the right hand side evaluated to 633.003352411 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 35.8249150205 volt but the right hand side evaluated to 35.8200284888 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.
Allowing negative dual variable(s) as small as -1.7386102375113117e-12.
Allowing negative dual variable(s) as small as -7.599120417307427e-12.
Allowing negative dual variable(s) as small as -2.1001047372080324e-11.
Allowing negative dual variable(s) as small as -3.854626945493935e-10.
Solving took 4 GP solves and 102 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 1024485.3691 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 103.179942839 ampere but the right hand side evaluated to 968.100387452 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 103.085313932 ampere but the right hand side evaluated to 968.100387738 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 102.957080712 ampere but the right hand side evaluated to 968.100387967 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 102.7611928 ampere but the right hand side evaluated to 968.100388234 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 102.455547046 ampere but the right hand side evaluated to 968.100388626 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 37.9241902627 volt but the right hand side evaluated to 37.1871391506 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 37.8575305347 volt but the right hand side evaluated to 37.1603750915 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 37.7564996933 volt but the right hand side evaluated to 37.113386751 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 37.6004397193 volt but the right hand side evaluated to 37.0394339287 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 37.3554427824 volt but the right hand side evaluated to 36.921372419 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 68.3448121854 ampere but the right hand side evaluated to 651.139527465 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 34.6911828859 volt but the right hand side evaluated to 34.6059417334 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 67.996785279 ampere but the right hand side evaluated to 647.904193966 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 34.7123281641 volt but the right hand side evaluated to 34.6316472961 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 67.6515392243 ampere but the right hand side evaluated to 644.688313422 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 34.7316271331 volt but the right hand side evaluated to 34.6551553476 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 67.304032778 ampere but the right hand side evaluated to 641.450438243 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 34.7523249547 volt but the right hand side evaluated to 34.6800781152 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 66.9538046083 ampere but the right hand side evaluated to 638.186327762 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 34.7746113162 volt but the right hand side evaluated to 34.7066152073 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 66.602783247 ampere but the right hand side evaluated to 634.911720155 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 34.7971035743 volt but the right hand side evaluated to 34.7332338413 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 66.2437581209 ampere but the right hand side evaluated to 631.565666238 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 34.8244224512 volt but the right hand side evaluated to 34.765001989 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 65.8831732426 ampere but the right hand side evaluated to 628.201721583 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 34.8522199504 volt but the right hand side evaluated to 34.7971224134 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 65.5188118588 ampere but the right hand side evaluated to 624.800811282 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 34.881837366 volt but the right hand side evaluated to 34.8310551631 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 65.1546871546 ampere but the right hand side evaluated to 621.396955638 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 34.9105538149 volt but the right hand side evaluated to 34.863830439 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 64.7736782467 ampere but the right hand side evaluated to 617.842516632 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 34.949381336 volt but the right hand side evaluated to 34.9073822892 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 64.3928184986 ampere but the right hand side evaluated to 614.28311208 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 34.9871296994 volt but the right hand side evaluated to 34.9495332444 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 64.0014192953 ampere but the right hand side evaluated to 610.625642915 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 35.0306108011 volt but the right hand side evaluated to 34.9976219096 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 63.6022848932 ampere but the right hand side evaluated to 606.893451658 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 35.0778847582 volt but the right hand side evaluated to 35.0495094122 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 63.1951367091 ampere but the right hand side evaluated to 603.083242209 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 35.1290119482 volt but the right hand side evaluated to 35.1052199226 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 62.7772565564 ampere but the right hand side evaluated to 599.170002101 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 35.1856186783 volt but the right hand side evaluated to 35.1664391562 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 62.3445497394 ampere but the right hand side evaluated to 595.115849867 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 35.2502009451 volt but the right hand side evaluated to 35.2357426073 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 61.8960757962 ampere but the right hand side evaluated to 590.910401488 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 35.3232191144 volt but the right hand side evaluated to 35.3135105896 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 61.4259478941 ampere but the right hand side evaluated to 586.498126203 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 35.4082781159 volt but the right hand side evaluated to 35.4033981075 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 22.7 seconds.
Allowing negative dual variable(s) as small as -2.505228e-11.
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 111.917836567 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 111.846567607 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 38.2100282197 volt but the right hand side evaluated to 37.7037161289 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 37.6768855588 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 73.392665092 ampere but the right hand side evaluated to 699.258596217 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 35.2477606648 volt but the right hand side evaluated to 35.1622394501 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 695.875655282 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 35.2658474049 volt but the right hand side evaluated to 35.1848241805 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 692.504956002 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 35.2825673788 volt but the right hand side evaluated to 35.2057709259 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 689.114827186 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 35.2279337562 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 35.3196688506 volt but the right hand side evaluated to 35.2514049371 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 682.279507696 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 35.3390293334 volt but the right hand side evaluated to 35.2748860483 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 35.3622193421 volt but the right hand side evaluated to 35.302537397 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 70.8211723156 ampere but the right hand side evaluated to 675.300203361 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 35.3857784245 volt but the right hand side evaluated to 35.3304204443 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 671.768432126 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 70.0653235173 ampere but the right hand side evaluated to 668.242005668 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 35.4342901639 volt but the right hand side evaluated to 35.3873031913 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 35.4249614402 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 69.2795660138 ampere but the right hand side evaluated to 660.909649986 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 35.4982003205 volt but the right hand side evaluated to 35.4604158798 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 68.8780121437 ampere but the right hand side evaluated to 657.160301283 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 35.5008174333 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 68.470500303 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 35.5437052115 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 35.6575533645 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.
Allowing negative dual variable(s) as small as -1.736422e-12.
Allowing negative dual variable(s) as small as -3.861184e-12.
Allowing negative dual variable(s) as small as -4.54102e-10.
Allowing negative dual variable(s) as small as -2.034659e-11.
Solving took 4 GP solves and 51.3 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 34.605934347 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 67.9967561254 ampere but the right hand side evaluated to 647.903698505 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 34.7123315534 volt but the right hand side evaluated to 34.6316722672 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 644.687989149 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 34.7316369761 volt but the right hand side evaluated to 34.6551478765 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 34.7523432016 volt but the right hand side evaluated to 34.6801111388 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 34.7746265947 volt but the right hand side evaluated to 34.7066185248 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 34.7332403725 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 631.565356649 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 34.8244247074 volt but the right hand side evaluated to 34.7650194097 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 628.201189495 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 34.8522256894 volt but the right hand side evaluated to 34.7971318045 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 624.800392363 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 34.8818626752 volt but the right hand side evaluated to 34.8310728915 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 65.1545408806 ampere but the right hand side evaluated to 621.395641572 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 34.9106171753 volt but the right hand side evaluated to 34.8639051744 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 64.7736574582 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 34.949389475 volt but the right hand side evaluated to 34.9074227946 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 64.3927468362 ampere but the right hand side evaluated to 614.282897541 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 34.9871552054 volt but the right hand side evaluated to 34.9495585361 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 610.625126092 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 35.0495305812 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 603.082751522 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 35.1290351229 volt but the right hand side evaluated to 35.1052318024 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 62.7772031245 ampere but the right hand side evaluated to 599.169547649 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 35.1856384229 volt but the right hand side evaluated to 35.1664476922 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 62.3445338826 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 61.8960274046 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 35.3232363173 volt but the right hand side evaluated to 35.3135031385 volt (Allowable error: 0.0001%, Actual error: 0.028%)

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 35.4082555295 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

Running tests...
----------------------------------------------------------------------
C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
  tau = np.exp(-0.175/costhsun)
......
----------------------------------------------------------------------
Ran 6 tests in 1363.810s

OK

Generating XML reports...
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in c:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in c:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz>=2011k in c:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy>=1.9.0 in c:\anaconda2\lib\site-packages (from pandas) (1.14.2)
Requirement already satisfied: six>=1.5 in c:\anaconda2\lib\site-packages (from python-dateutil->pandas) (1.11.0)
grin 1.2.1 requires argparse>=1.1, which is not installed.
Collecting git+https://github.com/hoburg/gpfit.git
  Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-0dkedt
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in c:\anaconda2\lib\site-packages
Requirement already satisfied: numpy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint>=0.7 in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in c:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-dl93gr\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse>=1.1, which is not installed.
Processing c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gplibrary
Requirement already satisfied: numpy>=1.12 in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in c:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1)
Building wheels for collected packages: gpkitmodels
  Running setup.py bdist_wheel for gpkitmodels: started
  Running setup.py bdist_wheel for gpkitmodels: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-drfizz\wheels\a3\80\70\6d80d6b876aaa160fc8dda3c238a4f64c571e65f335a009034
Successfully built gpkitmodels
grin 1.2.1 requires argparse>=1.1, which is not installed.
Installing collected packages: gpkitmodels
  Found existing installation: gpkitmodels 0.0.0.0
    Uninstalling gpkitmodels-0.0.0.0:
      Successfully uninstalled gpkitmodels-0.0.0.0
Successfully installed gpkitmodels-0.0.0.0
adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py'
adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py'
adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py'
adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py'
adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py'
Using solver 'mosek'
Solving for 11 variables.
Solving took 0.279 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.265 seconds.
Using solver 'mosek'
Solving for 8 variables.
Solving took 0.436 seconds.
Using solver 'mosek'
Solving for 24 variables.
Solving took 0.293 seconds.
Using solver 'mosek'
Solving for 24 variables.
Solving took 0.104 seconds.
Using solver 'mosek_cli'
Solving for 8 variables.
Solving took 0.398 seconds.
Using solver 'mosek_cli'
Solving for 24 variables.
Solving took 0.208 seconds.
Using solver 'mosek_cli'
Solving for 24 variables.
Solving took 0.358 seconds.
Using solver 'mosek'
Solving for 13 variables.
Solving took 0.091 seconds.
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.383 seconds.
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3838 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9776 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3883 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9590 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.4063 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.2552 but bound is 700000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000

Running tests...
----------------------------------------------------------------------
..........
----------------------------------------------------------------------
Ran 10 tests in 21.705s

OK

Generating XML reports...
Cloning into 'eVTOL'...
adding test for 'aircraft_models.py'

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 20.426s

OK

Generating XML reports...
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {})

calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'})

calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git']
  attempt 1

SETTINGS
defaultdict(<type 'str'>, {})


(venv2_gpkit) (base) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek>exit 0 
Build step 'Console output (build log) parsing' changed build result to FAILURE
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek' for the testing framework 'JUnit'.
[xUnit] [INFO] - Check 'Failed Tests' threshold.
[xUnit] [INFO] - Check 'Skipped Tests' threshold.
[xUnit] [INFO] - Setting the build status to FAILURE
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: FAILURE