protected DeorbitOptimizerBase(DeorbitAutopilot module, float dtol)
: base(module, dtol)
{
m = module;
inclination = 0f;
targetAlt = m.TargetAltitude;
}
public EccentricityOptimizer(DeorbitAutopilot module)
{
m = module;
comparer = new LTComparer(maneuver);
if (m.Body.atmosphere)
{
comparer.AddConditions(overheat);
}
comparer.AddConditions(steepness, fuel);
}
public EccentricityOptimizer(DeorbitAutopilot module)
{
m = module;
comparer = new LTComparer(maneuver, dR);
if (m.Body.atmosphere)
{
var maxDynP = C.MaxDynPressure * m.VSL.Torque.MaxPossible.AngularDragResistance;
comparer.AddConditions(overheat, steepness);
comparer.AddCondition(x => x.MaxDynamicPressure < maxDynP, (x, y) => x.MaxDynamicPressure < y.MaxDynamicPressure);
}
else
{
comparer.AddCondition(steepness);
}
comparer.AddCondition(fuel);
}
public DeorbitTrajectoryCorrector(DeorbitAutopilot module, float dtol)
: base(module, dtol)
{
prograde_dV = 0;
}
public DeorbitTrajectoryOptimizer(DeorbitAutopilot module, float dtol)
: base(module, dtol)
{
Ecc = m.initialEcc;
dEcc = Math.Max(Ecc / C.EccSteps, 0.05);
}
