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Include gravity in pilot accel calc when Vt < 1

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This commit is contained in:
tony 2002-09-29 14:13:39 +00:00
parent eb05a298e9
commit 09cb9b750c
1 changed files with 13 additions and 9 deletions
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22
src/FDM/JSBSim/FGAuxiliary.cpp
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@ -155,17 +155,21 @@ bool FGAuxiliary::Run()
vPilotAccel.InitMatrix();
if ( Translation->GetVt() > 1 ) {
vToEyePt = Aircraft->GetXYZep() - MassBalance->GetXYZcg();
vToEyePt *= inchtoft;
vPilotAccel = Aerodynamics->GetForces()
vPilotAccel = Aerodynamics->GetForces()
+ Propulsion->GetForces()
+ GroundReactions->GetForces();
vPilotAccel /= MassBalance->GetMass();
vPilotAccel += Rotation->GetPQRdot() * vToEyePt;
vPilotAccel += Rotation->GetPQR() * (Rotation->GetPQR() * vToEyePt);
//vPilotAccel(2)*=-1;
vPilotAccelN = vPilotAccel/Inertial->gravity();
}
vPilotAccel /= MassBalance->GetMass();
vToEyePt = Aircraft->GetXYZep() - MassBalance->GetXYZcg();
vToEyePt *= inchtoft;
vPilotAccel += Rotation->GetPQRdot() * vToEyePt;
vPilotAccel += Rotation->GetPQR() * (Rotation->GetPQR() * vToEyePt);
} else {
vPilotAccel = -1*( State->GetTl2b() * Inertial->GetGravity() );
}
vPilotAccelN = vPilotAccel/Inertial->gravity();
earthPosAngle += State->Getdt()*Inertial->omega();
return false;
} else {