public override bool Execute(FlightComputer f, FlightCtrlState fcs)
{
if (mAbort)
{
Mode = FlightMode.Off;
mAbort = false;
}
switch (Mode)
{
case FlightMode.Off:
break;
case FlightMode.KillRot:
FlightCore.HoldOrientation(fcs, f, Orientation * Quaternion.AngleAxis(90, Vector3.left));
break;
case FlightMode.AttitudeHold:
FlightCore.HoldAttitude(fcs, f, Frame, Attitude, Orientation);
break;
case FlightMode.AltitudeHold:
break;
}
return(false);
}
public override bool Execute(FlightComputer f, FlightCtrlState fcs)
{
if (RemainingDelta > 0)
{
var forward = Node.GetBurnVector(f.Vessel.orbit).normalized;
var up = (f.SignalProcessor.Body.position - f.SignalProcessor.Position).normalized;
var orientation = Quaternion.LookRotation(forward, up);
FlightCore.HoldOrientation(fcs, f, orientation);
double thrustToMass = (FlightCore.GetTotalThrust(f.Vessel) / f.Vessel.GetTotalMass());
if (thrustToMass == 0.0)
{
EngineActivated = false;
return(false);
}
EngineActivated = true;
fcs.mainThrottle = 1.0f;
RemainingTime = RemainingDelta / thrustToMass;
RemainingDelta -= thrustToMass * TimeWarp.deltaTime;
return(false);
}
f.Enqueue(AttitudeCommand.Off(), true, true, true);
return(true);
}
public override bool Pop(FlightComputer f)
{
var burn = f.ActiveCommands.FirstOrDefault(c => c is BurnCommand);
if (burn != null)
{
f.Remove(burn);
}
OriginalDelta = Node.DeltaV.magnitude;
RemainingDelta = Node.GetBurnVector(f.Vessel.orbit).magnitude;
EngineActivated = true;
double thrustToMass = FlightCore.GetTotalThrust(f.Vessel) / f.Vessel.GetTotalMass();
if (thrustToMass == 0.0)
{
EngineActivated = false;
RTUtil.ScreenMessage("[Flight Computer]: No engine to carry out the maneuver.");
}
else
{
RemainingTime = RemainingDelta / thrustToMass;
}
return(true);
}
public static ManeuverCommand WithNode(ManeuverNode node, FlightComputer f)
{
double thrust = FlightCore.GetTotalThrust(f.Vessel);
double advance = f.Delay;
if (thrust > 0)
{
advance += (node.DeltaV.magnitude / (thrust / f.Vessel.GetTotalMass())) / 2;
}
var newNode = new ManeuverCommand()
{
Node = new ManeuverNode()
{
DeltaV = node.DeltaV,
patch = node.patch,
solver = node.solver,
scaledSpaceTarget = node.scaledSpaceTarget,
nextPatch = node.nextPatch,
UT = node.UT,
nodeRotation = node.nodeRotation,
},
TimeStamp = node.UT - advance,
};
return(newNode);
}
public override bool Execute(FlightComputer f, FlightCtrlState fcs)
{
if (mAbort)
{
fcs.mainThrottle = 0.0f;
return(true);
}
if (Duration > 0)
{
fcs.mainThrottle = Throttle;
Duration -= TimeWarp.deltaTime;
}
else if (DeltaV > 0)
{
fcs.mainThrottle = Throttle;
DeltaV -= (Throttle * FlightCore.GetTotalThrust(f.Vessel) / f.Vessel.GetTotalMass()) * TimeWarp.deltaTime;
}
else
{
fcs.mainThrottle = 0.0f;
return(true);
}
return(false);
}
public override bool Pop(FlightComputer f)
{
var burn = f.ActiveCommands.FirstOrDefault(c => c is BurnCommand);
if (burn != null)
{
f.Remove(burn);
}
OriginalDelta = Node.DeltaV.magnitude;
RemainingDelta = Node.GetBurnVector(f.Vessel.orbit).magnitude;
RemainingTime = RemainingDelta / (FlightCore.GetTotalThrust(f.Vessel) / f.Vessel.GetTotalMass());
return(true);
}
