if(vt < 0.01) return 0;
xlo=xhi=0;
- xmin=fdmex->GetAircraft()->GetAlphaCLMin();
- xmax=fdmex->GetAircraft()->GetAlphaCLMax();
+ xmin=fdmex->GetAerodynamics()->GetAlphaCLMin();
+ xmax=fdmex->GetAerodynamics()->GetAlphaCLMax();
sfunc=&FGInitialCondition::GammaEqOfAlpha;
if(findInterval(0,guess)){
if(solve(&alpha,0)){
update_gear();
- stall_warning->setDoubleValue( Aircraft->GetStallWarn() );
+ stall_warning->setDoubleValue( Aerodynamics->GetStallWarn() );
/* elevator_pos_deg->setDoubleValue( FCS->GetDePos()*SG_RADIANS_TO_DEGREES );
left_aileron_pos_deg->setDoubleValue( FCS->GetDaLPos()*SG_RADIANS_TO_DEGREES );