public void keplerian3constraint(double sma, double ecc, double inc, bool omitCoast, bool targetInc)
{
if (status == PVGStatus.ENABLED)
{
return;
}
bool doupdate = false;
if (sma != old_sma || ecc != old_ecc)
{
doupdate = true;
}
// if we are tracking a target inc, don't reset
if (inc != old_inc && !targetInc)
{
doupdate = true;
}
if (p != null && p.bctype != BCType.KEPLER3)
{
doupdate = true;
}
if (p == null || doupdate)
{
if (p != null)
{
p.KillThread();
}
Debug.Log("[MechJeb] MechJebModuleGuidanceController: setting up keplerian3constraint");
PontryaginLaunch solver = NewPontryaginForLaunch(inc, sma);
solver.omitCoast = omitCoast;
solver.keplerian3constraint(sma, ecc, inc * UtilMath.Deg2Rad);
p = solver;
}
old_sma = sma;
old_ecc = ecc;
old_inc = inc;
}
public void keplerian3constraint(double sma, double ecc, double inc, bool omitCoast, bool currentInc)
{
if (status == PVGStatus.ENABLED)
{
return;
}
bool doupdate = false;
if (sma != old_sma || ecc != old_ecc)
{
doupdate = true;
}
// avoid slight drift in the current inclination from resetting guidance constantly
if (inc != old_inc && !currentInc)
{
doupdate = true;
}
if (p == null || doupdate)
{
if (p != null)
{
p.KillThread();
}
Debug.Log("[MechJeb] MechJebModuleGuidanceController: setting up keplerian3constraint");
PontryaginLaunch solver = NewPontryaginForLaunch(inc, sma);
solver.omitCoast = omitCoast;
solver.keplerian3constraint(sma, ecc, inc * UtilMath.Deg2Rad);
p = solver;
}
old_sma = sma;
old_ecc = ecc;
old_inc = inc;
}