diff --git a/src/FDM/JSBSim/FGInitialCondition.cpp b/src/FDM/JSBSim/FGInitialCondition.cpp index 43900ea95..16e37ca79 100644 --- a/src/FDM/JSBSim/FGInitialCondition.cpp +++ b/src/FDM/JSBSim/FGInitialCondition.cpp @@ -510,8 +510,8 @@ bool FGInitialCondition::getAlpha(void) { 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)){ diff --git a/src/FDM/JSBSim/JSBSim.cxx b/src/FDM/JSBSim/JSBSim.cxx index 95c81b037..753529405 100644 --- a/src/FDM/JSBSim/JSBSim.cxx +++ b/src/FDM/JSBSim/JSBSim.cxx @@ -553,7 +553,7 @@ bool FGJSBsim::copy_from_JSBsim() { 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 );