public IEnumerator <LandingTrajectory> GetEnumerator()
{
// m.Log("Calculating initial orbit eccentricity...");//debug
var tPos = m.CFG.Target.OrbPos(m.Body);
var UT = m.VSL.Physics.UT +
TrajectoryCalculator.AngleDelta(m.VesselOrbit, tPos, m.VSL.Physics.UT) / 360 * m.VesselOrbit.period;
if (UT < m.VSL.Physics.UT)
{
UT += m.VesselOrbit.period;
}
var vPos = m.VesselOrbit.getRelativePositionAtUT(UT);
var vVel = m.VesselOrbit.getOrbitalVelocityAtUT(UT);
var incl = Math.Abs(90 - Utils.Angle2(tPos, m.VesselOrbit.GetOrbitNormal()));
var ini_dV = TrajectoryCalculator.dV4Pe(m.VesselOrbit, (m.Body.Radius + m.TargetAltitude * 0.9), UT);
ini_dV = QuaternionD.AngleAxis(incl, vPos) * (ini_dV + vVel);
var dir = -ini_dV.normalized;
var maxV = ini_dV.magnitude;
ini_dV -= vVel;
Best = new LandingTrajectory(m.VSL, ini_dV, UT, m.CFG.Target, m.TargetAltitude);
yield return(Best);
//if there's not enough fuel, just go with the smallest maneuver possible
if (Best.FullManeuver)
{
//search for the best trajectory using current comparer
var start = Best;
var bestV = 0.0;
var dV = maxV / 10;
var V = dV;
while (Math.Abs(dV) > TrajectoryCalculator.C.dVtol)
{
var cur = new LandingTrajectory(m.VSL, start.ManeuverDeltaV + dir * V, start.StartUT, m.CFG.Target, start.TargetAltitude);
// m.Log("V {}, dV {}, is better {}\ncur {}\nbest {}",
// V, dV, comparer.isBetter(cur, Best), cur, Best);//debug
if (comparer.isBetter(cur, Best))
{
Best = cur;
bestV = V;
}
V += dV;
if (V < 0 || V > maxV || cur != Best)
{
dV /= -2.1;
V = bestV;
}
yield return(cur);
}
}
m.initialEcc = Best.Orbit.eccentricity;
// m.Log("initialEcc: {}", m.initialEcc);//debug
}
