public override void Init()
{
base.Init();
CFG.AP2.AddHandler(this, Autopilot2.ToOrbit);
ToOrbit.AttachTCA(TCA);
inclinationPID.setPID(C.InclinationPID);
}
public override void Init()
{
base.Init();
output_filter.Tau = C.LowPassF;
translation_pid.setPID(C.ManualThrust.PID);
needed_thrust_pid.setPID(C.NeededThrustPID);
CFG.HF.AddSingleCallback(ControlCallback);
}
public TargetedToOrbitExecutor()
{
pitch.setPID(C.TargetPitchPID);
pitch.Min = -AttitudeControlBase.C.MaxAttitudeError;
pitch.Max = 0;
throttle_correction.setPID(C.ThrottleCorrectionPID);
norm_correction.setClamp(AttitudeControlBase.C.MaxAttitudeError);
throttle_filter.Tau = 1;
angle2hor_filter.Tau = 1;
}
public ToOrbitExecutor() : base(null)
{
ErrorThreshold.Lower = ToOrbitAutopilot.C.Dtol / 10;
ErrorThreshold.Upper = ToOrbitAutopilot.C.Dtol;
pitch.setPID(C.PitchPID);
pitch.setClamp(AttitudeControlBase.C.MaxAttitudeError);
throttle.setPID(C.ThrottlePID);
throttle.setClamp(0.5f);
norm_correction.setPID(C.NormCorrectionPID);
norm_correction.setClamp(AttitudeControlBase.C.MaxAttitudeError);
TimeToApA.Value = TrajectoryCalculator.C.ManeuverOffset;
MinThrottle.Value = C.MinThrottle;
MaxG.Value = C.MaxG;
}
public void Init()
{
eStats = VSL.Engines.NoActiveEngines ?
VSL.Engines.GetNearestEnginedStageStats() :
VSL.Engines.GetEnginesStats(VSL.Engines.Active);
pitch.setPID(TargetedToOrbitExecutor.C.TargetPitchPID);
pitch.Min = -AttitudeControlBase.C.MaxAttitudeError;
pitch.Reset();
throttle.setPID(ToOrbitExecutor.C.ThrottlePID);
throttle.setClamp(0.5f);
throttle.Reset();
throttle_correction.setPID(TargetedToOrbitExecutor.C.ThrottleCorrectionPID);
throttle_correction.Reset();
correction_started.Reset();
}