Small console utility for predicting fligt dynamics of unpowered glider 5 dof (3 coordinates + pitch + roll)
node index state=225,0,0,0,0,15,14500,0,0,0 pitch=0 roll=0 tMax=10 dT=0.001 resSparse=50 Where:
- state - vector of initial trajectory params
- pitch - initial deflection of elevator
- roll - initial deflection of ailerons
- tMax - time of modelling interval
- dT - integration step
- resSparse - inerval between two points in result output
state layout - V, Th, Psi, epsZ, epsX, X, Y, Z, alpha, gamma
t, ...state layout, angle of elevator defletion, angle of aileron deflection