public VelPoint(AeroPredictor vessel, CelestialBody body, float altitude, float speed)
{
this.altitude = altitude;
this.speed = speed;
AeroPredictor.Conditions conditions = new AeroPredictor.Conditions(body, speed, altitude);
float gravParameter, radius;
lock (body)
{
gravParameter = (float)body.gravParameter;
radius = (float)body.Radius;
}
this.mach = conditions.mach;
this.dynamicPressure = 0.0005f * conditions.atmDensity * speed * speed;
float weight = (vessel.Mass * gravParameter / ((radius + altitude) * (radius + altitude))) - (vessel.Mass * speed * speed / (radius + altitude));
Vector3 thrustForce = vessel.GetThrustForce(conditions);
AoA_max = vessel.GetMaxAoA(conditions, out Lift_max);
AoA_level = Mathf.Min(vessel.GetAoA(conditions, weight), AoA_max);
pitchInput = vessel.GetPitchInput(conditions, AoA_level);
Thrust_available = thrustForce.magnitude;
Vector3 force = vessel.GetAeroForce(conditions, AoA_level, pitchInput);
drag = AeroPredictor.GetDragForceMagnitude(force, AoA_level);
Thrust_excess = -drag - AeroPredictor.GetDragForceMagnitude(thrustForce, AoA_level);
Accel_excess = Thrust_excess / vessel.Mass / WindTunnelWindow.gAccel;
LDRatio = Mathf.Abs(AeroPredictor.GetLiftForceMagnitude(force, AoA_level) / drag);
dLift = (vessel.GetLiftForceMagnitude(conditions, AoA_level + WindTunnelWindow.AoAdelta, pitchInput) -
vessel.GetLiftForceMagnitude(conditions, AoA_level, pitchInput)) / (WindTunnelWindow.AoAdelta * Mathf.Rad2Deg);
}
public EnvelopePoint(AeroPredictor vessel, CelestialBody body, float altitude, float speed, float AoA_guess = float.NaN, float maxA_guess = float.NaN, float pitchI_guess = float.NaN)
{
this.altitude = altitude;
this.speed = speed;
AeroPredictor.Conditions conditions = new AeroPredictor.Conditions(body, speed, altitude);
float gravParameter, radius;
lock (body)
{
gravParameter = (float)body.gravParameter;
radius = (float)body.Radius;
}
this.mach = conditions.mach;
this.dynamicPressure = 0.0005f * conditions.atmDensity * speed * speed;
float weight = (vessel.Mass * gravParameter / ((radius + altitude) * (radius + altitude))); // TODO: Minus centrifugal force...
Vector3 thrustForce = vessel.GetThrustForce(conditions);
//AoA_max = vessel.GetMaxAoA(conditions, out Lift_max, maxA_guess);
if (float.IsNaN(maxA_guess))
{
AoA_max = vessel.GetMaxAoA(conditions, out Lift_max, maxA_guess);
}
else
{
AoA_max = maxA_guess;
Lift_max = AeroPredictor.GetLiftForceMagnitude(vessel.GetAeroForce(conditions, AoA_max, 1) + thrustForce, AoA_max);
}
AoA_level = vessel.GetAoA(conditions, weight, guess: AoA_guess, pitchInputGuess: 0, lockPitchInput: true);
if (AoA_level < AoA_max)
{
pitchInput = vessel.GetPitchInput(conditions, AoA_level, guess: pitchI_guess);
}
else
{
pitchInput = 1;
}
Thrust_available = thrustForce.magnitude;
force = vessel.GetAeroForce(conditions, AoA_level, pitchInput);
liftforce = AeroPredictor.ToFlightFrame(force, AoA_level); //vessel.GetLiftForce(body, speed, altitude, AoA_level, mach, atmDensity);
drag = AeroPredictor.GetDragForceMagnitude(force, AoA_level);
float lift = AeroPredictor.GetLiftForceMagnitude(force, AoA_level);
Thrust_excess = -drag - AeroPredictor.GetDragForceMagnitude(thrustForce, AoA_level);
if (weight > Lift_max)// AoA_level >= AoA_max)
{
Thrust_excess = Lift_max - weight;
AoA_level = AoA_max;
}
Accel_excess = (Thrust_excess / vessel.Mass / WindTunnelWindow.gAccel);
LDRatio = Mathf.Abs(lift / drag);
dLift = (vessel.GetLiftForceMagnitude(conditions, AoA_level + WindTunnelWindow.AoAdelta, pitchInput) -
vessel.GetLiftForceMagnitude(conditions, AoA_level, pitchInput)) / (WindTunnelWindow.AoAdelta * Mathf.Rad2Deg);
}
public EnvelopePoint(AeroPredictor vessel, CelestialBody body, float altitude, float speed, float AoA_guess = float.NaN, float maxA_guess = float.NaN, float pitchI_guess = float.NaN)
{
this.altitude = altitude;
this.speed = speed;
AeroPredictor.Conditions conditions = new AeroPredictor.Conditions(body, speed, altitude);
float gravParameter, radius;
gravParameter = (float)body.gravParameter;
radius = (float)body.Radius;
this.mach = conditions.mach;
this.dynamicPressure = 0.0005f * conditions.atmDensity * speed * speed;
float weight = (vessel.Mass * gravParameter / ((radius + altitude) * (radius + altitude))) - (vessel.Mass * speed * speed / (radius + altitude));
Vector3 thrustForce = vessel.GetThrustForce(conditions);
fuelBurnRate = vessel.GetFuelBurnRate(conditions);
//AoA_max = vessel.GetMaxAoA(conditions, out Lift_max, maxA_guess);
if (float.IsNaN(maxA_guess))
{
AoA_max = vessel.GetMaxAoA(conditions, out Lift_max, maxA_guess);
//Lift_max = AeroPredictor.GetLiftForceMagnitude(vessel.GetAeroForce(conditions, AoA_max, 1) + thrustForce, AoA_max);
}
else
{
AoA_max = maxA_guess;
Lift_max = AeroPredictor.GetLiftForceMagnitude(vessel.GetAeroForce(conditions, AoA_max, 1) + thrustForce, AoA_max);
}
AoA_level = vessel.GetAoA(conditions, weight, guess: AoA_guess, pitchInputGuess: 0, lockPitchInput: true);
if (AoA_level < AoA_max)
{
pitchInput = vessel.GetPitchInput(conditions, AoA_level, guess: pitchI_guess);
}
else
{
pitchInput = 1;
}
if (speed < 5 && Math.Abs(altitude) < 10)
{
AoA_level = 0;
}
Thrust_available = thrustForce.magnitude;
//vessel.GetAeroCombined(conditions, AoA_level, pitchInput, out force, out Vector3 torque);
force = vessel.GetAeroForce(conditions, AoA_level, pitchInput);
aeroforce = AeroPredictor.ToFlightFrame(force, AoA_level); //vessel.GetLiftForce(body, speed, altitude, AoA_level, mach, atmDensity);
drag = -aeroforce.z;
float lift = aeroforce.y;
Thrust_excess = -drag - AeroPredictor.GetDragForceMagnitude(thrustForce, AoA_level);
if (weight > Lift_max)// AoA_level >= AoA_max)
{
Thrust_excess = Lift_max - weight;
AoA_level = AoA_max;
}
Accel_excess = (Thrust_excess / vessel.Mass / WindTunnelWindow.gAccel);
LDRatio = Math.Abs(lift / drag);
dLift = (vessel.GetLiftForceMagnitude(conditions, AoA_level + WindTunnelWindow.AoAdelta, pitchInput) - lift)
/ (WindTunnelWindow.AoAdelta * Mathf.Rad2Deg);
//stabilityDerivative = (vessel.GetAeroTorque(conditions, AoA_level + WindTunnelWindow.AoAdelta, pitchInput).x - torque.x)
// / (WindTunnelWindow.AoAdelta * Mathf.Rad2Deg);
//GetStabilityValues(vessel, conditions, AoA_level, out stabilityRange, out stabilityScore);
completed = true;
}