/* track prograde out of the atmosphere */
private AttitudeState AttitudePrograde()
{
if (vessel.altitude > mainBody.RealMaxAtmosphereAltitude() && orbit.ApA > target_altitude)
{
return(AttitudeState.EXIT);
}
double pitch = pitchPID.Update(adjustedTimeToAp(), 0, 0, 30);
attitude.attitudeTo(Quaternion.AngleAxis((float)pitch, Vector3.left) * Vector3d.forward, AttitudeReference.SURFACE_HORIZONTAL);
return(AttitudeState.PROGRADE);
}
/*
* Throttle State Machine
*/
/* burn to raise and maintain Ap at intermediate altitude */
private ThrottleState ThrottleLaunch()
{
if (orbit.ApA > intermediate_altitude)
{
warp.WarpAtPhysicsRate(this, 4, true);
throttle.target = 0.0;
if (adjustedTimeToAp() < targetAPtime)
{
return(ThrottleState.FINAL);
}
}
else
{
warp.WarpAtPhysicsRate(this, 0, true);
if (vessel.dynamicPressurekPa < maxQlimit)
{
throttlePID.ResetI();
}
throttle.target = throttlePID.Update(vessel.dynamicPressurekPa, maxQlimit, 0, 1);
}
return(ThrottleState.LAUNCH);
}
