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Fade out the turbulence within two wingspans of the ground.

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david 2003-02-12 18:34:39 +00:00
parent 4ecd146258
commit 9f5498acf4
1 changed files with 14 additions and 3 deletions
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17
src/FDM/JSBSim/FGAtmosphere.cpp
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@ -261,7 +261,7 @@ void FGAtmosphere::Calculate(double altitude)
void FGAtmosphere::Turbulence(void)
{
switch (turbType) {
case ttBerndt:
case ttBerndt: {
vDirectiondAccelDt(eX) = 1 - 2.0*(((double)(rand()))/RAND_MAX);
vDirectiondAccelDt(eY) = 1 - 2.0*(((double)(rand()))/RAND_MAX);
vDirectiondAccelDt(eZ) = 1 - 2.0*(((double)(rand()))/RAND_MAX);
@ -271,14 +271,24 @@ void FGAtmosphere::Turbulence(void)
MagnitudeAccel += MagnitudedAccelDt*rate*State->Getdt();
Magnitude += MagnitudeAccel*rate*State->Getdt();
// Fade the magnitude within two wingspans
// of the ground (WAG)
double AdjustedMagnitude = Magnitude;
double AdjustedMagnitudeAccel = MagnitudeAccel;
double HOverBMAC = Position->GetHOverBMAC();
if (HOverBMAC < 2.0) {
AdjustedMagnitude *= (HOverBMAC / 2.0);
AdjustedMagnitudeAccel *= (HOverBMAC / 2.0);
}
vDirectiondAccelDt.Normalize();
vDirectionAccel += vDirectiondAccelDt*rate*State->Getdt();
vDirectionAccel.Normalize();
vDirection += vDirectionAccel*rate*State->Getdt();
vDirection.Normalize();
vTurbulence = TurbGain*Magnitude * vDirection;
vTurbulenceGrad = TurbGain*MagnitudeAccel * vDirection;
vTurbulence = TurbGain*AdjustedMagnitude * vDirection;
vTurbulenceGrad = TurbGain*AdjustedMagnitudeAccel * vDirection;
vBodyTurbGrad = State->GetTl2b()*vTurbulenceGrad;
vTurbPQR(eP) = vBodyTurbGrad(eY)/Aircraft->GetWingSpan();
@ -293,6 +303,7 @@ void FGAtmosphere::Turbulence(void)
vTurbPQR(eR) = vBodyTurbGrad(eX)/10.0;
break;
}
default:
break;
}