private void updateNode()
{
Vector2 nodePosition = node.getNodePosition();
bool nodeTowardsPerigee = OrbitalHelper.towardsPerigeeOrbit(mouseTrueAnomaly, shipElements.Clockwise);
double nodeSpeed = OrbitalHelper.calculateSpeed(nodePosition, shipElements.SemiMajorAxis, shipElements.Mu, shipElements.OrbitType);
double nodeVelocityAngle = OrbitalHelper.calculateVelocityAngle(nodePosition, shipElements.Eccentricity, shipElements.SemiMajorAxis, mouseTrueAnomaly, shipElements.GlobalRotationAngle, shipElements.Clockwise, nodeTowardsPerigee, shipElements.OrbitType);
Vector2 nodeVelocity = OrbitalHelper.assembleVelocityVector(nodeVelocityAngle, nodeSpeed);
GravityElementsClass newOrbit = calculateInitialOrbitalElements(nodePosition, nodeVelocity + thrustVector, shipElements.massiveBody);
node = new Node(newOrbit, mouseTrueAnomaly, nodePosition);
patchedConics.updatePotentialEncounters(node.getManeuver());
}
private void calculateNextOrbitalElements()
{
//update timestep
gravityElements.TimeStep = GlobalElements.timeStep;
//Adjust tranformation vector
gravityElements.GlobalTransformationVector = gravityElements.MassiveBody.transform.position;
//Calculate next meanAnomaly
gravityElements.MeanAnomaly = OrbitalHelper.calculateMeanAnomaly(gravityElements.Eccentricity, gravityElements.SemiMajorAxis, gravityElements.AnomalyAtEpoch,
gravityElements.TimeStep, gravityElements.TimeAtEpoch, gravityElements.Clockwise, gravityElements.Mu, gravityElements.OrbitType);
//Calculate Eccentric Anomaly
gravityElements.EccentricAnomaly = OrbitalHelper.calculateEccentricAnomaly(gravityElements.Eccentricity, gravityElements.SemiMajorAxis, GlobalElements.GRAV_CONST, gravityElements.TimeStep, gravityElements.TimeAtEpoch,
gravityElements.MeanAnomaly, gravityElements.EccentricAnomaly, gravityElements.Mu, gravityElements.Clockwise, gravityElements.OrbitType);
//CalculateTrueAnomaly
gravityElements.TrueAnomaly = OrbitalHelper.calculateTrueAnomaly(gravityElements.Eccentricity, gravityElements.EccentricAnomaly, gravityElements.MeanAnomaly, gravityElements.OrbitType);
//Calculate Altitude
gravityElements.Altitude = OrbitalHelper.calculateAltitude(gravityElements.Eccentricity, gravityElements.SemiMajorAxis, gravityElements.SemiLatusRectum, gravityElements.TrueAnomaly, gravityElements.OrbitType);
//Calculate positionVector
gravityElements.Position = OrbitalHelper.calculatePosition(gravityElements.Perigee, gravityElements.TrueAnomaly, gravityElements.GlobalRotationAngle, gravityElements.Altitude, gravityElements.OrbitType);
//Are we going towards the perigee?
gravityElements.TowardsPerigee = OrbitalHelper.towardsPerigeeOrbit(gravityElements.MeanAnomaly, gravityElements.Clockwise);
//Calculate velocity angle
gravityElements.VelocityAngle = OrbitalHelper.calculateVelocityAngle(gravityElements.Position, gravityElements.Eccentricity, gravityElements.SemiMajorAxis,
gravityElements.TrueAnomaly, gravityElements.GlobalRotationAngle, gravityElements.Clockwise, gravityElements.TowardsPerigee, gravityElements.OrbitType);
//Calculate Speed
gravityElements.Speed = OrbitalHelper.calculateSpeed(gravityElements.Position, gravityElements.SemiMajorAxis, gravityElements.Mu, gravityElements.OrbitType);
//Calculate Velocity
gravityElements.velocity = OrbitalHelper.assembleVelocityVector(gravityElements.VelocityAngle, gravityElements.Speed);
//advance epoch
gravityElements.AnomalyAtEpoch = gravityElements.MeanAnomaly;
//Advance time
gravityElements.TimeAtEpoch = OrbitalHelper.advanceTime(gravityElements.TimeAtEpoch, gravityElements.TimeStep, gravityElements.Clockwise, gravityElements.OrbitType);
}
public void advanceToFutureState(double time)
{
//update timestep
this.TimeStep = time;
//Adjust tranformation vector
this.GlobalTransformationVector = this.MassiveBody.transform.position;
//Calculate next meanAnomaly
this.MeanAnomaly = OrbitalHelper.calculateMeanAnomaly(this.Eccentricity, this.SemiMajorAxis, this.AnomalyAtEpoch,
this.TimeStep, this.TimeAtEpoch, this.Clockwise, this.Mu, this.OrbitType);
//Calculate Eccentric Anomaly
this.EccentricAnomaly = OrbitalHelper.calculateEccentricAnomaly(this.Eccentricity, this.SemiMajorAxis, GlobalElements.GRAV_CONST, this.TimeStep, this.TimeAtEpoch,
this.MeanAnomaly, this.EccentricAnomaly, this.Mu, this.Clockwise, this.OrbitType);
//CalculateTrueAnomaly
this.TrueAnomaly = OrbitalHelper.calculateTrueAnomaly(this.Eccentricity, this.EccentricAnomaly, this.MeanAnomaly, this.OrbitType);
//Calculate Altitude
this.Altitude = OrbitalHelper.calculateAltitude(this.Eccentricity, this.SemiMajorAxis, this.SemiLatusRectum, this.TrueAnomaly, this.OrbitType);
//Calculate positionVector
this.Position = OrbitalHelper.calculatePosition(this.Perigee, this.TrueAnomaly, this.GlobalRotationAngle, this.Altitude, this.OrbitType);
//Are we going towards the perigee?
this.TowardsPerigee = OrbitalHelper.towardsPerigeeOrbit(this.MeanAnomaly, this.Clockwise);
//Calculate velocity angle
this.VelocityAngle = OrbitalHelper.calculateVelocityAngle(this.Position, this.Eccentricity, this.SemiMajorAxis,
this.TrueAnomaly, this.GlobalRotationAngle, this.Clockwise, this.TowardsPerigee, this.OrbitType);
//Calculate Speed
this.Speed = OrbitalHelper.calculateSpeed(this.Position, this.SemiMajorAxis, this.Mu, this.OrbitType);
//Calculate Velocity
this.velocity = OrbitalHelper.assembleVelocityVector(this.VelocityAngle, this.Speed);
//advance epoch
this.AnomalyAtEpoch = this.MeanAnomaly;
//Advance time
this.TimeAtEpoch = OrbitalHelper.advanceTime(this.TimeAtEpoch, this.TimeStep, this.Clockwise, this.OrbitType);
}
public Tuple <Vector2, Vector2> calculateLocalPositionAndVelocityAtFutureTime(double timeStep)
{
//Calculate time at epoch
double timeAtEpoch = OrbitalHelper.advanceTime(this.timeAtEpoch, timeStep, clockwise, orbitType);
//Calculate next meanAnomaly
double meanAnomaly = OrbitalHelper.calculateMeanAnomaly(eccentricity, semiMajorAxis, anomalyAtEpoch,
timeStep, timeAtEpoch, clockwise, mu, orbitType);
//Calculate Eccentric Anomaly
double eccentricAnomaly = OrbitalHelper.calculateEccentricAnomaly(eccentricity, semiMajorAxis, GlobalElements.GRAV_CONST, timeStep, timeAtEpoch,
meanAnomaly, this.eccentricAnomaly, mu, clockwise, orbitType);
//CalculateTrueAnomaly
double trueAnomaly = OrbitalHelper.calculateTrueAnomaly(eccentricity, eccentricAnomaly, meanAnomaly, orbitType);
//Calculate Altitude
double altitude = OrbitalHelper.calculateAltitude(eccentricity, semiMajorAxis, semiLatusRectum, trueAnomaly, orbitType);
//Calculate positionVector
Vector2 position = OrbitalHelper.calculatePosition(perigee, trueAnomaly, globalRotationAngle, altitude, orbitType);
//Are we going towards the perigee?
bool towardsPerigee = OrbitalHelper.towardsPerigeeOrbit(meanAnomaly, clockwise);
//Calculate velocity angle
double velocityAngle = OrbitalHelper.calculateVelocityAngle(position, eccentricity, semiMajorAxis,
trueAnomaly, globalRotationAngle, clockwise, towardsPerigee, orbitType);
//Calculate Speed
double speed = OrbitalHelper.calculateSpeed(position, semiMajorAxis, mu, orbitType);
//Calculate Velocity
Vector2 velocity = OrbitalHelper.assembleVelocityVector(velocityAngle, speed);
//Im returning the position here, you know, just in case you couldnt figure it out on your own
return(new Tuple <Vector2, Vector2>(position, velocity));
}