Jim Wilson wrote: > > Andy, I dumped the last 3 iterations (for my own benifit) and following that > is the solution report. What I did for now was go into the Airplain.cpp
Airplain -> Airplane ? > Drag factor: 1.000199 > Lift Factor: 1.000410 > aoaDelta: 0.000110 > tailDelta: 0.000083 > elevDelta: 0.000114 > Drag factor: 1.000475 > Lift Factor: 1.000451 > aoaDelta: 0.000100 > tailDelta: 0.000986 > elevDelta: 0.000095 > Drag factor: 1.000276 > Lift Factor: 1.000042 > aoaDelta: 0.000010 > tailDelta: 0.001069 > elevDelta: 0.000018 tailDelta is increasing here. At a guess, I'd say maybe the solution is oscillating. > YASim solution results: > Iterations: 10002 > Drag Coefficient: 12.3517 > Lift Ratio: 85.8242 > Cruise AoA: 2.97772 > Tail Incidence: -4.82189 > Approach Elevator: -0.714202 > CG: -29.5, -0.0, 1.3 > YASim SOLUTION FAILURE: > Solution failed to converge after 10000 iterations[ > - Julian _______________________________________________ Flightgear-devel mailing list [EMAIL PROTECTED] http://mail.flightgear.org/mailman/listinfo/flightgear-devel
