public void FixedUpdate()
{
if (HighLogic.LoadedSceneIsEditor)
{
return;
}
if (engine.type == EngineWrapper.EngineType.NONE || !engine.EngineIgnited)
{
return;
}
if ((!vessel.mainBody.atmosphereContainsOxygen && useOxygen) || part.vessel.altitude > vessel.mainBody.maxAtmosphereAltitude)
{
engine.SetThrust(0);
return;
}
Vector3d V = vessel.srf_velocity;
Vector3d t = part.FindModelTransform(engine.thrustVectorTransformName).forward.normalized;
vx = (float)Vector3d.Cross(V, t).magnitude;
vz = -(float)Vector3d.Dot(V, t);
float density = (float)ferram4.FARAeroUtil.GetCurrentDensity(part.vessel.mainBody, (float)part.vessel.altitude);
aje.calc(density, vx, vz, weight * 9.801f);
engine.SetThrust(aje.lift / 1000f);
float isp = aje.lift / 9.801f / BSFC / aje.power;
engine.SetIsp(isp);
ShaftPower = ((int)(aje.power / 745.7f)).ToString() + "HP";
if (sas != null)
{
float sasMultiplier = aje.lift / weight / 9.801f;
if (sasMultiplier < 0)
{
sasMultiplier = 0;
}
sas.PitchTorque = sasP * sasMultiplier;
sas.YawTorque = sasY * sasMultiplier;
sas.RollTorque = sasR * sasMultiplier;
}
}
public void FixedUpdate()
{
if (HighLogic.LoadedSceneIsEditor)
{
return;
}
if (engine.type == EngineWrapper.EngineType.NONE || !engine.EngineIgnited)
{
return;
}
if (vessel.mainBody.atmosphereContainsOxygen == false || part.vessel.altitude > vessel.mainBody.maxAtmosphereAltitude)
{
engine.SetThrust(0);
return;
}
#region Inlet
float Arearatio, OverallTPR = 0, EngineArea = 0, InletArea = 0;
AJEModule e;
AJEInlet i;
foreach (Part p in vessel.parts)
{
if (p.Modules.Contains("AJEModule"))
{
e = (AJEModule)p.Modules["AJEModule"];
EngineArea += (float)(e.aje.areaCore * (1 + e.aje.byprat));
}
if (p.Modules.Contains("AJEInlet"))
{
i = (AJEInlet)p.Modules["AJEInlet"];
if (true)
{
InletArea += i.Area;
OverallTPR += i.Area * i.cosine * i.cosine * i.GetTPR((float)aje.fsmach);
}
}
}
if (InletArea > 0)
{
OverallTPR /= InletArea;
}
Arearatio = Mathf.Min(InletArea / EngineArea, 1f);
aje.eta[2] = Mathf.Clamp(Mathf.Sqrt(Arearatio) * OverallTPR, 0.001f, 1f);
Inlet = "Area:" + ((int)(Arearatio * 100f)).ToString() + "% TPR:" + ((int)(OverallTPR * 100f)).ToString() + "%";
#endregion
aje.FARps0 = FlightGlobals.getStaticPressure(vessel.altitude, vessel.mainBody);
aje.FARts0 = FlightGlobals.getExternalTemperature((float)vessel.altitude, vessel.mainBody) + 273.15f;
Environment = (((int)(aje.FARps0 * 100f)) / 100f).ToString() + "atm;" + (((int)(aje.FARts0 * 100f)) / 100f) + "K";
if (usePrat3Curve)
{
aje.prat[3] = aje.p3p2d = (double)(prat3Curve.Evaluate((float)aje.fsmach));
}
aje.u0d = part.vessel.srfSpeed * 3.6d;
OverallThrottle = vessel.ctrlState.mainThrottle * engine.thrustPercentage / 100f;
if (!useAB)
{
aje.comPute();
engine.SetThrust(((float)aje.forceNetlb) * 0.004448f);
engine.SetIsp((float)aje.isp);
Mode = "Cruise " + System.Convert.ToString((int)(OverallThrottle * 100f)) + "%";
}
else
{
if (OverallThrottle <= ABthreshold)
{
engine.useEngineResponseTime = true;
aje.abflag = 0;
aje.comPute();
engine.SetThrust(((float)aje.forceNetlb) * 0.004448f / ABthreshold);
engine.SetIsp((float)aje.isp);
Mode = "Cruise " + System.Convert.ToString((int)(OverallThrottle / ABthreshold * 100f)) + "%";
}
else
{
// only allow instance response when already at max RPM; if the compressor is still spooling up, it's still spooling up.
if (engine.currentThrottle > ABthreshold)
{
engine.useEngineResponseTime = false;
}
else
{
engine.useEngineResponseTime = true;
}
aje.abflag = 1;
aje.tt7 = (OverallThrottle - ABthreshold) * (ABmax - ABmin) / (1 - ABthreshold) + ABmin;
aje.comPute();
engine.SetThrust(((float)aje.forceNetlb) * 0.004448f / OverallThrottle);
engine.SetIsp((float)aje.isp * ABIspMult);
Mode = "Afterburner " + System.Convert.ToString((int)((OverallThrottle - ABthreshold) / (1 - ABthreshold) * 100f)) + "%";
}
}
Mode += " (" + (aje.forceGrosslb * 0.004448f).ToString("N2") + "kN gr)";
if (aje.fireflag > 0.9f && useOverheat)
{
part.temperature = (aje.fireflag * 2f - 1.2f) * part.maxTemp;
}
fireflag = aje.fireflag;
parttemp = part.temperature;
maxtemp = part.maxTemp;
// mach = (float)aje.fsmach;
}