void CalcLambertDVs(double t0, double dt, out Vector3d exitDV, out Vector3d captureDV)
{
double t1 = t0 + dt;
CelestialBody origin_planet = origin.referenceBody;
Vector3d V1_0 = origin_planet.orbit.getOrbitalVelocityAtUT(t0);
Vector3d R1 = origin_planet.orbit.getRelativePositionAtUT(t0);
Vector3d R2 = destination.getRelativePositionAtUT(t1);
Vector3d V2_1 = destination.getOrbitalVelocityAtUT(t1);
Vector3d V1 = V1_0;
Vector3d V2 = V2_1;
try {
GoodingSolver.Solve(origin_planet.referenceBody.gravParameter, R1, V1_0, R2, V2_1, dt, 0, out V1, out V2);
}
catch (Exception) {}
exitDV = V1 - V1_0;
captureDV = V2_1 - V2;
}
void ComputeDeltaV(object args)
{
CelestialBody origin_planet = origin.referenceBody;
for (int date_index = TakeDateIndex();
date_index >= 0;
date_index = TakeDateIndex())
{
double t0 = DateFromIndex(date_index);
if (double.IsInfinity(t0))
{
continue;
}
Vector3d V1_0 = origin_planet.orbit.getOrbitalVelocityAtUT(t0);
Vector3d R1 = origin_planet.orbit.getRelativePositionAtUT(t0);
int duration_samples = DurationSamplesForDate(date_index);
for (int duration_index = 0; duration_index < duration_samples; duration_index++)
{
if (stop)
{
break;
}
double dt = DurationFromIndex(duration_index);
double t1 = t0 + dt;
Vector3d R2 = destination.getRelativePositionAtUT(t1);
Vector3d V2_1 = destination.getOrbitalVelocityAtUT(t1);
/* bool short_way = Vector3d.Dot(Vector3d.Cross(R1, R2), origin_planet.orbit.GetOrbitNormal()) > 0; */
try
{
Vector3d V1, V2;
#if DEBUG
log[date_index, duration_index] = dt + ","
+ R1.x + "," + R1.y + "," + R1.z + ","
+ R2.x + "," + R2.y + "," + R2.z + ","
+ V1_0.x + "," + V1_0.y + "," + V1_0.z;
#endif
/* LambertSolver.Solve(R1, R2, dt, origin_planet.referenceBody, short_way, out V1, out V2); */
GoodingSolver.Solve(R1, V1_0, R2, V2_1, dt, origin_planet.referenceBody, 0, out V1, out V2);
#if DEBUG
log[date_index, duration_index] += "," + V1.x + "," + V1.y + "," + V1.z;
#endif
Vector3d soi_exit_velocity = V1 - V1_0;
var maneuver = ComputeEjectionManeuver(soi_exit_velocity, origin, t0);
if (!double.IsNaN(maneuver.dV.sqrMagnitude) && !double.IsNaN(maneuver.UT))
{
computed[date_index, duration_index] = maneuver;
}
#if DEBUG
log[date_index, duration_index] += "," + maneuver.dV.magnitude;
#endif
}
catch (Exception) {}
}
}
JobFinished();
}