Skipping 324 KB.. Full Log

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 64.7129854974 ampere but the right hand side evaluated to 616.978166826 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 35.1035551369 volt but the right hand side evaluated to 35.0441897724 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 64.384756038 ampere but the right hand side evaluated to 613.919685369 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 35.1346923257 volt but the right hand side evaluated to 35.0795902433 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 64.4216341138 ampere but the right hand side evaluated to 614.260158859 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 35.1286434391 volt but the right hand side evaluated to 35.0728724463 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 64.0819022158 ampere but the right hand side evaluated to 611.092339255 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 35.1617733456 volt but the right hand side evaluated to 35.1103262358 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 64.1265000144 ampere but the right hand side evaluated to 611.506025709 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 35.1555273573 volt but the right hand side evaluated to 35.1033807043 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 63.7763662138 ampere but the right hand side evaluated to 608.237981375 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 35.1898729056 volt but the right hand side evaluated to 35.1420300386 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 63.826802066 ampere but the right hand side evaluated to 608.708634292 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 35.1846321508 volt but the right hand side evaluated to 35.1361603465 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 63.4514298364 ampere but the right hand side evaluated to 605.210803703 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 35.229903912 volt but the right hand side evaluated to 35.1864427668 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 63.5247124372 ampere but the right hand side evaluated to 605.886453403 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 35.2144375912 volt but the right hand side evaluated to 35.1695568011 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 63.144539985 ampere but the right hand side evaluated to 602.336301536 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 35.2571367815 volt but the right hand side evaluated to 35.2169164309 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 63.2111078447 ampere but the right hand side evaluated to 602.959629185 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 35.2508597532 volt but the right hand side evaluated to 35.209922544 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 62.8219642234 ampere but the right hand side evaluated to 599.320241349 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 35.2936659788 volt but the right hand side evaluated to 35.2572158975 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 62.8995939093 ampere but the right hand side evaluated to 600.046386431 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%)

Warning: Constraint [v_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [V]... >= Kv_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.2848593394 volt but the right hand side evaluated to 35.247517411 volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [i_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [A]... >= 9.55*i0_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.4925640875 ampere but the right hand side evaluated to 596.23920042 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 35.3335689604 volt but the right hand side evaluated to 35.3009389389 volt (Allowable error: 0.0001%, Actual error: 0.092%)

Warning: Constraint [i_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [A]... >= 9.55*i0_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 62.5797452168 ampere but the right hand side evaluated to 597.055226584 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 35.3232000432 volt but the right hand side evaluated to 35.2895904826 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 62.1577661828 ampere but the right hand side evaluated to 593.105231639 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 35.3758186562 volt but the right hand side evaluated to 35.3469640258 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 62.251654354 ampere but the right hand side evaluated to 593.986187527 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 35.3657237533 volt but the right hand side evaluated to 35.3359357358 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 61.8067005818 ampere but the right hand side evaluated to 589.82100695 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 35.4274235854 volt but the right hand side evaluated to 35.4027024435 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 61.9157118512 ampere but the right hand side evaluated to 590.841979203 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 35.4120778493 volt but the right hand side evaluated to 35.3861408227 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 61.4491979521 ampere but the right hand side evaluated to 586.472829971 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 35.4818573196 volt but the right hand side evaluated to 35.4611638971 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 61.5712565186 ampere but the right hand side evaluated to 587.616010218 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 35.4626012965 volt but the right hand side evaluated to 35.4405296886 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 61.0866148758 ampere but the right hand side evaluated to 583.072424558 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 35.5381461153 volt but the right hand side evaluated to 35.5212960561 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 61.2160880052 ampere but the right hand side evaluated to 584.287757126 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 35.5186349024 volt but the right hand side evaluated to 35.5004763002 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 60.7002929035 ampere but the right hand side evaluated to 579.450656544 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 35.6083517735 volt but the right hand side evaluated to 35.5957366124 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 60.8470703194 ampere but the right hand side evaluated to 580.827876707 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 35.582124198 volt but the right hand side evaluated to 35.5679684242 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 60.3004262618 ampere but the right hand side evaluated to 575.697401848 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 35.6857224151 volt but the right hand side evaluated to 35.6772663806 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 60.4635186658 ampere but the right hand side evaluated to 577.228706713 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%)

Warning: Constraint [v_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [V]... >= Kv_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 35.6534125162 volt but the right hand side evaluated to 35.6432829346 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 59.8790144364 ampere but the right hand side evaluated to 571.737928607 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 35.7753516377 volt but the right hand side evaluated to 35.7710908553 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 60.0603432495 ampere but the right hand side evaluated to 573.442195642 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 35.7357034054 volt but the right hand side evaluated to 35.7296644303 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 59.6316053621 ampere but the right hand side evaluated to 569.411333459 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 35.8327215534 volt but the right hand side evaluated to 35.8308262602 volt (Allowable error: 0.0001%, Actual error: 0.0053%)

Using solver 'mosek'
Solving for 4713 variables.
Solving took 1.42 seconds.
Allowing negative dual variable(s) as small as -2.460121464987749e-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 111.917791222 ampere but the right hand side evaluated to 1056.06638219 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 111.846524942 ampere but the right hand side evaluated to 1056.0663822 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 111.750507045 ampere but the right hand side evaluated to 1056.06638221 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 111.604586227 ampere but the right hand side evaluated to 1056.06638223 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 111.378514433 ampere but the right hand side evaluated to 1056.06638225 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 38.2100141126 volt but the right hand side evaluated to 37.7037012849 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 38.1552336822 volt but the right hand side evaluated to 37.6768749425 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 38.0707728691 volt but the right hand side evaluated to 37.6300622827 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 37.940140873 volt but the right hand side evaluated to 37.5563494891 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 37.7350492737 volt but the right hand side evaluated to 37.4386740918 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 73.3928153969 ampere but the right hand side evaluated to 699.25961863 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 35.2476969344 volt but the right hand side evaluated to 35.1621624897 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 73.028796094 ampere but the right hand side evaluated to 695.87541755 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 35.2658426892 volt but the right hand side evaluated to 35.184844783 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 72.666913913 ampere but the right hand side evaluated to 692.504815388 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 35.282567842 volt but the right hand side evaluated to 35.2057872309 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 72.3030606812 ampere but the right hand side evaluated to 689.115067121 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 35.3004680961 volt but the right hand side evaluated to 35.2279254162 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 71.9368493591 ampere but the right hand side evaluated to 685.702602055 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 35.3196731023 volt but the right hand side evaluated to 35.251396385 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 71.5698137742 ampere but the right hand side evaluated to 682.279420702 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 35.3390626302 volt but the right hand side evaluated to 35.2749383533 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 71.1962560662 ampere but the right hand side evaluated to 678.79866768 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 35.3622116264 volt but the right hand side evaluated to 35.3025339285 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 70.8211478493 ampere but the right hand side evaluated to 675.300285773 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 35.3857694351 volt but the right hand side evaluated to 35.3304278995 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 70.4426128096 ampere but the right hand side evaluated to 671.768491056 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 35.4108302373 volt but the right hand side evaluated to 35.3598300535 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 70.0653041569 ampere but the right hand side evaluated to 668.241691755 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 35.4342936942 volt but the right hand side evaluated to 35.3873078903 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 69.6718398023 ampere but the right hand side evaluated to 664.574016979 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 35.4671566502 volt but the right hand side evaluated to 35.424971572 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 69.2795560172 ampere but the right hand side evaluated to 660.909760009 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 35.4981977023 volt but the right hand side evaluated to 35.4604261997 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 68.8780050816 ampere but the right hand side evaluated to 657.160303786 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 35.5339486321 volt but the right hand side evaluated to 35.5008260568 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 68.4704776029 ampere but the right hand side evaluated to 653.352603847 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 35.5721784807 volt but the right hand side evaluated to 35.5436927045 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 68.056557728 ampere but the right hand side evaluated to 649.482386358 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 35.6130177107 volt but the right hand side evaluated to 35.5891405818 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 67.6342784979 ampere but the right hand side evaluated to 645.531838157 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 35.6575669285 volt but the right hand side evaluated to 35.6383277155 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 67.20079711 ampere but the right hand side evaluated to 641.475055758 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 35.7074578231 volt but the right hand side evaluated to 35.6929616665 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 66.7558912433 ampere but the right hand side evaluated to 637.308552523 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 35.7626614741 volt but the right hand side evaluated to 35.7529388603 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 66.2964784697 ampere but the right hand side evaluated to 633.003351797 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 35.824915062 volt but the right hand side evaluated to 35.8200285337 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500
Using solver 'mosek'
Solving for 571 variables.
Solving took 0.265 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 111.917804703 ampere but the right hand side evaluated to 1056.06638069 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 111.846524027 ampere but the right hand side evaluated to 1056.06638072 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 111.750484113 ampere but the right hand side evaluated to 1056.06638076 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 111.604534577 ampere but the right hand side evaluated to 1056.0663808 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 111.378430324 ampere but the right hand side evaluated to 1056.06638085 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 38.210097543 volt but the right hand side evaluated to 37.7037016972 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 38.1553062636 volt but the right hand side evaluated to 37.6768748813 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 38.0708297734 volt but the right hand side evaluated to 37.6300614964 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 37.9401763172 volt but the right hand side evaluated to 37.5563477568 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 37.7350572404 volt but the right hand side evaluated to 37.4386712873 volt (Allowable error: 0.0001%, Actual error: 0.79%)

Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500
Using solver 'mosek'
Solving for 571 variables.
Solving took 0.25 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 111.917804467 ampere but the right hand side evaluated to 1056.06638043 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 111.846523843 ampere but the right hand side evaluated to 1056.06638046 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 111.750483991 ampere but the right hand side evaluated to 1056.06638049 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 111.604534535 ampere but the right hand side evaluated to 1056.06638054 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 111.378430369 ampere but the right hand side evaluated to 1056.06638059 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 38.210097434 volt but the right hand side evaluated to 37.7037016889 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 38.1553061782 volt but the right hand side evaluated to 37.6768748746 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 38.0708297158 volt but the right hand side evaluated to 37.6300614918 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 37.9401762953 volt but the right hand side evaluated to 37.5563477548 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 37.735057258 volt but the right hand side evaluated to 37.438671288 volt (Allowable error: 0.0001%, Actual error: 0.79%)

Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0349 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0382 but bound is 0.0500
Using solver 'mosek'
Solving for 4713 variables.
Solving took 1.34 seconds.
Allowing negative dual variable(s) as small as -2.4585903142154306e-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 111.917791407 ampere but the right hand side evaluated to 1056.06638239 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 111.846525088 ampere but the right hand side evaluated to 1056.0663824 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 111.750507143 ampere but the right hand side evaluated to 1056.06638241 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 111.604586267 ampere but the right hand side evaluated to 1056.06638243 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 111.37851441 ampere but the right hand side evaluated to 1056.06638244 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 38.2100141814 volt but the right hand side evaluated to 37.703701292 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 38.155233735 volt but the right hand side evaluated to 37.6768749484 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 38.0707729026 volt but the right hand side evaluated to 37.6300622871 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 37.9401408824 volt but the right hand side evaluated to 37.5563494915 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 37.7350492577 volt but the right hand side evaluated to 37.4386740922 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 73.3926809116 ampere but the right hand side evaluated to 699.258557554 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 35.2477854549 volt but the right hand side evaluated to 35.1622627069 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 73.0288051595 ampere but the right hand side evaluated to 695.875491323 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 35.2658369296 volt but the right hand side evaluated to 35.1848383584 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 72.6669135015 ampere but the right hand side evaluated to 692.504815503 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 35.2825684801 volt but the right hand side evaluated to 35.2057880879 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 72.3030615206 ampere but the right hand side evaluated to 689.11507658 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 35.3004678441 volt but the right hand side evaluated to 35.2279252458 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 71.9368495626 ampere but the right hand side evaluated to 685.702606413 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 35.3196732686 volt but the right hand side evaluated to 35.2513966845 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 71.5698616586 ampere but the right hand side evaluated to 682.279811323 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 35.3390316562 volt but the right hand side evaluated to 35.2749037968 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 71.1962560162 ampere but the right hand side evaluated to 678.798669419 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 35.3622118997 volt but the right hand side evaluated to 35.3025343247 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 70.8211475835 ampere but the right hand side evaluated to 675.300285447 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 35.3857698179 volt but the right hand side evaluated to 35.3304284055 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 70.4426114826 ampere but the right hand side evaluated to 671.768481914 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 35.410831304 volt but the right hand side evaluated to 35.3598313155 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 70.0653003715 ampere but the right hand side evaluated to 668.241661239 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 35.4342962472 volt but the right hand side evaluated to 35.3873107567 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 69.6718396765 ampere but the right hand side evaluated to 664.574016953 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 35.4671568529 volt but the right hand side evaluated to 35.4249718418 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 69.2795550643 ampere but the right hand side evaluated to 660.909752808 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 35.4981984127 volt but the right hand side evaluated to 35.4604270175 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 68.8780050248 ampere but the right hand side evaluated to 657.160304095 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 35.5339487655 volt but the right hand side evaluated to 35.5008262389 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 68.4704776908 ampere but the right hand side evaluated to 653.352605165 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 35.572178497 volt but the right hand side evaluated to 35.5436927486 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 68.0565577969 ampere but the right hand side evaluated to 649.482387357 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 35.6130177214 volt but the right hand side evaluated to 35.5891406125 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 67.6342785815 ampere but the right hand side evaluated to 645.531839156 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 35.6575669151 volt but the right hand side evaluated to 35.638327714 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 67.2007975186 ampere but the right hand side evaluated to 641.475059472 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 35.7074575912 volt but the right hand side evaluated to 35.6929614238 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 66.7560008911 ampere but the right hand side evaluated to 637.30951848 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 35.7625930787 volt but the right hand side evaluated to 35.7528656694 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 66.2964786446 ampere but the right hand side evaluated to 633.003353371 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 35.8249149635 volt but the right hand side evaluated to 35.8200284295 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 -1.7387760639606161e-12.
Allowing negative dual variable(s) as small as -6.9056013362414765e-12.
Allowing negative dual variable(s) as small as -2.104701294446915e-11.
Allowing negative dual variable(s) as small as -4.724184255027228e-10.
Solving took 4 GP solves and 10.8 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 1024485.3945 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 103.179836331 ampere but the right hand side evaluated to 968.100424244 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 103.085230956 ampere but the right hand side evaluated to 968.10042453 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 102.957026457 ampere but the right hand side evaluated to 968.100424758 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 102.761175505 ampere but the right hand side evaluated to 968.100425017 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 102.455570505 ampere but the right hand side evaluated to 968.100425408 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 37.9241470946 volt but the right hand side evaluated to 37.1871350622 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 37.8574977847 volt but the right hand side evaluated to 37.1603717818 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 37.756479549 volt but the right hand side evaluated to 37.1133843915 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 37.600435537 volt but the right hand side evaluated to 37.0394327928 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 37.3554555633 volt but the right hand side evaluated to 36.9213726341 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 68.3444958663 ampere but the right hand side evaluated to 651.135097744 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 34.69118636 volt but the right hand side evaluated to 34.6058648197 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 67.9966558621 ampere but the right hand side evaluated to 647.90146936 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 34.7122271862 volt but the right hand side evaluated to 34.6314614195 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 67.6514105721 ampere but the right hand side evaluated to 644.68575426 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 34.7315431713 volt but the right hand side evaluated to 34.6549950663 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 67.3039042779 ampere but the right hand side evaluated to 641.448032984 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 34.7522578489 volt but the right hand side evaluated to 34.6799430247 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 66.9537015151 ampere but the right hand side evaluated to 638.18427662 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 34.7745434125 volt but the right hand side evaluated to 34.7064854385 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 66.60259401 ampere but the right hand side evaluated to 634.909075814 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 34.7971067798 volt but the right hand side evaluated to 34.7331880063 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 66.2436899066 ampere but the right hand side evaluated to 631.564174221 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 34.8243616102 volt but the right hand side evaluated to 34.7648918466 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 65.8831600676 ampere but the right hand side evaluated to 628.200816361 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 34.8521367267 volt but the right hand side evaluated to 34.7969932953 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 65.5186758642 ampere but the right hand side evaluated to 624.798974585 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 34.8818473747 volt but the right hand side evaluated to 34.8310330738 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 65.155900944 ampere but the right hand side evaluated to 621.406798102 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 34.9096971851 volt but the right hand side evaluated to 34.8628714621 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 64.7737145013 ampere but the right hand side evaluated to 617.842361949 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 34.9493028513 volt but the right hand side evaluated to 34.9072737835 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 64.3931310795 ampere but the right hand side evaluated to 614.285449089 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 34.9868828049 volt but the right hand side evaluated to 34.9492475852 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 64.0013423493 ampere but the right hand side evaluated to 610.624678281 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 35.0306258146 volt but the right hand side evaluated to 34.997622828 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 63.6022383664 ampere but the right hand side evaluated to 606.892825386 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 35.0778888833 volt but the right hand side evaluated to 35.0495023099 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 63.1951011265 ampere but the right hand side evaluated to 603.082774367 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 35.1290165875 volt but the right hand side evaluated to 35.1052165939 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 62.777224319 ampere but the right hand side evaluated to 599.169615555 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 35.1856275387 volt but the right hand side evaluated to 35.1664430669 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 62.3445359325 ampere but the right hand side evaluated to 595.115670102 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 35.2502032573 volt but the right hand side evaluated to 35.2357418785 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 61.8960694395 ampere but the right hand side evaluated to 590.910320908 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 35.3232206426 volt but the right hand side evaluated to 35.3135108397 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 61.4259476557 ampere but the right hand side evaluated to 586.4981187 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 35.4082774929 volt but the right hand side evaluated to 35.4033971213 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2113 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0257 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0393 but bound is 0.0500
Using solver 'mosek_cli'
Solving for 4713 variables.
Solving took 1.42 seconds.
Allowing negative dual variable(s) as small as -2.47299e-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 73.3929586632 ampere but the right hand side evaluated to 699.260565081 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 35.247619674 volt but the right hand side evaluated to 35.1620526968 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 35.2058037337 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 72.3030996278 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 35.2279361422 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 35.2749189614 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 -1.780457e-12.
Allowing negative dual variable(s) as small as -4.329714e-12.
Allowing negative dual variable(s) as small as -4.498308e-10.
Allowing negative dual variable(s) as small as -4.545695e-10.
Solving took 4 GP solves and 12 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 103.179789945 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 103.085217445 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 37.9241457401 volt but the right hand side evaluated to 37.1871375583 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 37.8574958035 volt but the right hand side evaluated to 37.1603773974 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 37.7564755979 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 68.3444937291 ampere but the right hand side evaluated to 651.135377022 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 34.6058583691 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 67.996620132 ampere but the right hand side evaluated to 647.901278782 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 34.7122274166 volt but the right hand side evaluated to 34.6314734533 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 67.6513966746 ampere but the right hand side evaluated to 644.685582289 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 34.7315675129 volt but the right hand side evaluated to 34.6550137212 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 67.3038875857 ampere but the right hand side evaluated to 641.448077642 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 34.752273697 volt but the right hand side evaluated to 34.6799444017 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 66.9536775214 ampere but the right hand side evaluated to 638.184540188 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 34.774522271 volt but the right hand side evaluated to 34.7064841175 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 66.6025589846 ampere but the right hand side evaluated to 634.909201449 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 34.7971330581 volt but the right hand side evaluated to 34.7332012435 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 66.2436757545 ampere but the right hand side evaluated to 631.564179463 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 34.8243550586 volt but the right hand side evaluated to 34.764886908 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 628.200604266 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 34.852155985 volt but the right hand side evaluated to 34.7970013128 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 65.5186608147 ampere but the right hand side evaluated to 624.79864688 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 34.8310358983 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 65.1559091403 ampere but the right hand side evaluated to 621.406631729 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 34.909709511 volt but the right hand side evaluated to 34.8628707892 volt (Allowable error: 0.0001%, Actual error: 0.13%)

Warning: Constraint [i_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 64.7737222319 ampere but the right hand side evaluated to 617.842352999 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%)

Warning: Constraint [v_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 34.9493195763 volt but the right hand side evaluated to 34.9072610831 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 64.3931331938 ampere but the right hand side evaluated to 614.28518279 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 34.9868753093 volt but the right hand side evaluated to 34.9492430415 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 64.001338679 ampere but the right hand side evaluated to 610.624558439 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 35.0306362483 volt but the right hand side evaluated to 34.9976210916 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 606.892642463 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%)

Warning: Constraint [v_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.0778893875 volt but the right hand side evaluated to 35.0494976305 volt (Allowable error: 0.0001%, Actual error: 0.081%)

Warning: Constraint [i_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 63.195114756 ampere but the right hand side evaluated to 603.082751522 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 35.1289999939 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 61.8960893007 ampere but the right hand side evaluated to 590.910211685 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%)

Warning: Constraint [v_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [V]... >= Kv_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 35.3232363173 volt but the right hand side evaluated to 35.3135051811 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 35.4082909378 volt but the right hand side evaluated to 35.4033923764 volt (Allowable error: 0.0001%, Actual error: 0.014%)

Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2113 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0257 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0393 but bound is 0.0500

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 460.166s

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-4ascsg
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-2oheno\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-f_re2h\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 0.033 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 0.083 seconds.
Using solver 'mosek'
Solving for 8 variables.
Solving took 0.021 seconds.
Using solver 'mosek'
Solving for 24 variables.
Solving took 0.022 seconds.
Using solver 'mosek'
Solving for 24 variables.
Solving took 0.02 seconds.
Using solver 'mosek_cli'
Solving for 8 variables.
Solving took 0.081 seconds.
Using solver 'mosek_cli'
Solving for 24 variables.
Solving took 0.081 seconds.
Using solver 'mosek_cli'
Solving for 24 variables.
Solving took 0.115 seconds.
Using solver 'mosek'
Solving for 13 variables.
Solving took 0.027 seconds.
Using solver 'mosek_cli'
Solving for 13 variables.
Solving took 0.087 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 6.070s

OK

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

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 2.098s

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 
[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 SUCCESS
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: SUCCESS