public ReentrySimulation(Orbit _initialOrbit, double _UT, SimulatedVessel _vessel, SimCurves _simcurves, IDescentSpeedPolicy _descentSpeedPolicy, double _decelEndAltitudeASL, double _maxThrustAccel, double _parachuteSemiDeployMultiplier, double _probableLandingSiteASL, bool _multiplierHasError, double _dt, double _min_dt)
{
// Store all the input values as they were given
input_initialOrbit = _initialOrbit;
input_UT = _UT;
vessel = _vessel;
input_descentSpeedPolicy = _descentSpeedPolicy;
input_decelEndAltitudeASL = _decelEndAltitudeASL;
input_maxThrustAccel = _maxThrustAccel;
input_parachuteSemiDeployMultiplier = _parachuteSemiDeployMultiplier;
input_probableLandingSiteASL = _probableLandingSiteASL;
input_multiplierHasError = _multiplierHasError;
input_dt = _dt;
// the vessel attitude relative to the surface vel. Fixed for now
attitude = Quaternion.Euler(180,0,0);
min_dt = _min_dt;
max_dt = _dt;
dt = max_dt;
// Get a copy of the original orbit, to be more thread safe
initialOrbit = new Orbit();
initialOrbit.UpdateFromOrbitAtUT(_initialOrbit, _UT, _initialOrbit.referenceBody);
CelestialBody body = _initialOrbit.referenceBody;
bodyHasAtmosphere = body.atmosphere;
bodyRadius = body.Radius;
gravParameter = body.gravParameter;
this.parachuteSemiDeployMultiplier = _parachuteSemiDeployMultiplier;
this.multiplierHasError = _multiplierHasError;
bodyAngularVelocity = body.angularVelocity;
this.descentSpeedPolicy = _descentSpeedPolicy;
decelRadius = bodyRadius + _decelEndAltitudeASL;
aerobrakedRadius = bodyRadius + body.RealMaxAtmosphereAltitude();
mainBody = body;
this.maxThrustAccel = _maxThrustAccel;
this.probableLandingSiteASL = _probableLandingSiteASL;
this.probableLandingSiteRadius = _probableLandingSiteASL + bodyRadius;
referenceFrame = ReferenceFrame.CreateAtCurrentTime(_initialOrbit.referenceBody);
orbitReenters = OrbitReenters(_initialOrbit);
if (orbitReenters)
startUT = _UT;
maxDragGees = 0;
deltaVExpended = 0;
trajectory = new List<AbsoluteVector>();
simCurves = _simcurves;
once = true;
}
private static void Reset(SimCurves obj)
{
}
public void Init(Orbit _initialOrbit, double _UT, SimulatedVessel _vessel, SimCurves _simcurves, IDescentSpeedPolicy _descentSpeedPolicy, double _decelEndAltitudeASL, double _maxThrustAccel, double _parachuteSemiDeployMultiplier, double _probableLandingSiteASL, bool _multiplierHasError, double _dt, double _min_dt, double _maxOrbits, bool _noSKiptoFreefall)
{
// Store all the input values as they were given
input_initialOrbit = _initialOrbit;
input_UT = _UT;
vessel = _vessel;
input_descentSpeedPolicy = _descentSpeedPolicy;
input_decelEndAltitudeASL = _decelEndAltitudeASL;
input_maxThrustAccel = _maxThrustAccel;
input_parachuteSemiDeployMultiplier = _parachuteSemiDeployMultiplier;
input_probableLandingSiteASL = _probableLandingSiteASL;
input_multiplierHasError = _multiplierHasError;
input_dt = _dt;
// the vessel attitude relative to the surface vel. Fixed for now
attitude = Quaternion.Euler(180,0,0);
min_dt = _min_dt;
max_dt = _dt;
dt = max_dt;
steps = 0;
maxOrbits = _maxOrbits;
noSKiptoFreefall = _noSKiptoFreefall;
// Get a copy of the original orbit, to be more thread safe
//initialOrbit = new Orbit();
initialOrbit.UpdateFromOrbitAtUT(_initialOrbit, _UT, _initialOrbit.referenceBody);
CelestialBody body = _initialOrbit.referenceBody;
bodyHasAtmosphere = body.atmosphere;
bodyRadius = body.Radius;
gravParameter = body.gravParameter;
this.parachuteSemiDeployMultiplier = _parachuteSemiDeployMultiplier;
this.multiplierHasError = _multiplierHasError;
bodyAngularVelocity = body.angularVelocity;
this.descentSpeedPolicy = _descentSpeedPolicy;
decelRadius = bodyRadius + _decelEndAltitudeASL;
aerobrakedRadius = bodyRadius + body.RealMaxAtmosphereAltitude();
mainBody = body;
this.maxThrustAccel = _maxThrustAccel;
this.probableLandingSiteASL = _probableLandingSiteASL;
this.probableLandingSiteRadius = _probableLandingSiteASL + bodyRadius;
referenceFrame.UpdateAtCurrentTime(_initialOrbit.referenceBody);
orbitReenters = OrbitReenters(_initialOrbit);
startX = initialOrbit.SwappedRelativePositionAtUT(startUT);
// This calls some Unity function so it should be done outside the thread
if (orbitReenters)
{
startUT = _UT;
t = startUT;
AdvanceToFreefallEnd(initialOrbit);
}
maxDragGees = 0;
deltaVExpended = 0;
trajectory = ListPool<AbsoluteVector>.Instance.Borrow();
simCurves = _simcurves;
once = true;
}
public static ReentrySimulation Borrow(Orbit _initialOrbit, double _UT, SimulatedVessel _vessel, SimCurves _simcurves, IDescentSpeedPolicy _descentSpeedPolicy, double _decelEndAltitudeASL, double _maxThrustAccel, double _parachuteSemiDeployMultiplier, double _probableLandingSiteASL, bool _multiplierHasError, double _dt, double _min_dt, double _maxOrbits, bool _noSKiptoFreefall)
{
ReentrySimulation sim = pool.Borrow();
sim.Init(_initialOrbit, _UT, _vessel, _simcurves, _descentSpeedPolicy, _decelEndAltitudeASL, _maxThrustAccel, _parachuteSemiDeployMultiplier, _probableLandingSiteASL, _multiplierHasError, _dt, _min_dt, _maxOrbits, _noSKiptoFreefall);
return sim;
}
public ReentrySimulation(Orbit _initialOrbit, double _UT, SimulatedVessel _vessel, SimCurves _simcurves, IDescentSpeedPolicy _descentSpeedPolicy, double _decelEndAltitudeASL, double _maxThrustAccel, double _parachuteSemiDeployMultiplier, double _probableLandingSiteASL, bool _multiplierHasError, double _dt, double _min_dt)
{
// Store all the input values as they were given
input_initialOrbit = _initialOrbit;
input_UT = _UT;
vessel = _vessel;
input_descentSpeedPolicy = _descentSpeedPolicy;
input_decelEndAltitudeASL = _decelEndAltitudeASL;
input_maxThrustAccel = _maxThrustAccel;
input_parachuteSemiDeployMultiplier = _parachuteSemiDeployMultiplier;
input_probableLandingSiteASL = _probableLandingSiteASL;
input_multiplierHasError = _multiplierHasError;
input_dt = _dt;
// the vessel attitude relative to the surface vel. Fixed for now
attitude = Quaternion.Euler(180, 0, 0);
min_dt = _min_dt;
max_dt = _dt;
dt = max_dt;
// Get a copy of the original orbit, to be more thread safe
initialOrbit = new Orbit();
initialOrbit.UpdateFromOrbitAtUT(_initialOrbit, _UT, _initialOrbit.referenceBody);
CelestialBody body = _initialOrbit.referenceBody;
bodyHasAtmosphere = body.atmosphere;
bodyRadius = body.Radius;
gravParameter = body.gravParameter;
this.parachuteSemiDeployMultiplier = _parachuteSemiDeployMultiplier;
this.multiplierHasError = _multiplierHasError;
bodyAngularVelocity = body.angularVelocity;
this.descentSpeedPolicy = _descentSpeedPolicy;
decelRadius = bodyRadius + _decelEndAltitudeASL;
aerobrakedRadius = bodyRadius + body.RealMaxAtmosphereAltitude();
mainBody = body;
this.maxThrustAccel = _maxThrustAccel;
this.probableLandingSiteASL = _probableLandingSiteASL;
this.probableLandingSiteRadius = _probableLandingSiteASL + bodyRadius;
referenceFrame = ReferenceFrame.CreateAtCurrentTime(_initialOrbit.referenceBody);
orbitReenters = OrbitReenters(_initialOrbit);
if (orbitReenters)
{
startUT = _UT;
}
maxDragGees = 0;
deltaVExpended = 0;
trajectory = new List <AbsoluteVector>();
simCurves = _simcurves;
once = true;
}
