private void UpdateVP()
{
List <Part> ActiveEngines = new List <Part>();
ActiveEngines = GetListOfActivatedEngines(AV);
VP.FlightStatus = (byte)AV.situation;
//Orbit
VP.CurrentOrbit = OrbUtil.GetOrbitData(AV.orbit);
VP.VVI = (float)AV.verticalSpeed;
VP.G = (float)AV.geeForce;
double ASL = AV.mainBody.GetAltitude(AV.CoM);
double AGL = (ASL - AV.terrainAltitude);
if (AGL < ASL)
{
VP.RAlt = (float)AGL;
}
else
{
VP.RAlt = (float)ASL;
}
VP.Alt = (float)ASL;
VP.Vsurf = (float)AV.srfSpeed;
VP.Lat = (float)AV.latitude;
VP.Lon = (float)AV.longitude;
TempR = GetResourceTotal(AV, "LiquidFuel");
VP.LiquidFuelTot = TempR.Max;
VP.LiquidFuel = TempR.Current;
VP.LiquidFuelTotS = (float)ProspectForResourceMax("LiquidFuel", ActiveEngines);
VP.LiquidFuelS = (float)ProspectForResource("LiquidFuel", ActiveEngines);
TempR = GetResourceTotal(AV, "Oxidizer");
VP.OxidizerTot = TempR.Max;
VP.Oxidizer = TempR.Current;
VP.OxidizerTotS = (float)ProspectForResourceMax("Oxidizer", ActiveEngines);
VP.OxidizerS = (float)ProspectForResource("Oxidizer", ActiveEngines);
TempR = GetResourceTotal(AV, "ElectricCharge");
VP.EChargeTot = TempR.Max;
VP.ECharge = TempR.Current;
TempR = GetResourceTotal(AV, "MonoPropellant");
VP.MonoPropTot = TempR.Max;
VP.MonoProp = TempR.Current;
TempR = GetResourceTotal(AV, "IntakeAir");
VP.IntakeAirTot = TempR.Max;
VP.IntakeAir = TempR.Current;
TempR = GetResourceTotal(AV, "SolidFuel");
VP.SolidFuelTot = TempR.Max;
VP.SolidFuel = TempR.Current;
TempR = GetResourceTotal(AV, "XenonGas");
VP.XenonGasTot = TempR.Max;
VP.XenonGas = TempR.Current;
VP.MissionTime = (float)AV.missionTime;
VP.UT = (float)Planetarium.GetUniversalTime();
VP.VOrbit = (float)AV.orbit.GetVel().magnitude;
VP.MNTime = 0;
VP.MNDeltaV = 0;
VP.TargetDist = 0;
VP.TargetV = 0;
VP.HasTarget = (byte)(HasTarget() ? 1 : 0);
//mathy stuff
Quaternion rotationSurface;
CoM = AV.CoM;
up = (CoM - AV.mainBody.position).normalized;
north = Vector3d.Exclude(up, (AV.mainBody.position + AV.mainBody.transform.up * (float)AV.mainBody.Radius) - CoM).normalized;
east = Vector3d.Cross(up, north);
rotationSurface = Quaternion.LookRotation(north, up);
Vector3d attitude = Quaternion.Inverse(Quaternion.Euler(90, 0, 0) * Quaternion.Inverse(AV.GetTransform().rotation) * rotationSurface).eulerAngles;
VP.Roll = (float)((attitude.z > 180) ? (attitude.z - 360.0) : attitude.z);
VP.Pitch = (float)((attitude.x > 180) ? (360.0 - attitude.x) : -attitude.x);
VP.Heading = (float)attitude.y;
Vector3d prograde = new Vector3d(0, 0, 0);
switch (FlightGlobals.speedDisplayMode)
{
case FlightGlobals.SpeedDisplayModes.Surface:
prograde = AV.srf_velocity.normalized;
break;
case FlightGlobals.SpeedDisplayModes.Orbit:
prograde = AV.obt_velocity.normalized;
break;
case FlightGlobals.SpeedDisplayModes.Target:
prograde = FlightGlobals.ship_tgtVelocity;
break;
}
VP.Prograde = WorldVecToNavHeading(up, north, east, prograde);
if (HasTarget())
{
ITargetable t = AV.targetObject;
VP.Target = WorldVecToNavHeading(up, north, east, t.GetTransform().position - AV.transform.position);
VP.TargetDist = (float)Vector3.Distance(t.GetTransform().position, AV.transform.position);
VP.TargetV = (float)FlightGlobals.ship_tgtVelocity.magnitude;
if (t is Vessel)
{
attitude = Quaternion.Inverse(Quaternion.Euler(90, 0, 0) * Quaternion.Inverse(t.GetVessel().GetTransform().rotation) * rotationSurface).eulerAngles;
VP.TargetRotation.Pitch = (float)((attitude.x > 180) ? (360.0 - attitude.x) : -attitude.x);
VP.TargetRotation.Heading = (float)attitude.y;
}
else if (t is ModuleDockingNode)
{
VP.TargetRotation = WorldVecToNavHeading(up, north, east, t.GetFwdVector());
}
}
if (AV.patchedConicSolver != null)
{
if (AV.patchedConicSolver.maneuverNodes != null)
{
if (AV.patchedConicSolver.maneuverNodes.Count > 0)
{
VP.MNTime = (UInt32)Math.Round(AV.patchedConicSolver.maneuverNodes[0].UT - Planetarium.GetUniversalTime());
VP.MNDeltaV = (float)AV.patchedConicSolver.maneuverNodes[0].GetBurnVector(AV.patchedConicSolver.maneuverNodes[0].patch).magnitude; //Added JS
VP.Maneuver = WorldVecToNavHeading(up, north, east, AV.patchedConicSolver.maneuverNodes[0].GetBurnVector(AV.patchedConicSolver.maneuverNodes[0].patch));
}
}
}
VP.MainControls = CalcMainControls();
VP.ActionGroups = CalcActionGroups();
VP.MaxOverHeat = GetMaxOverHeat(AV);
VP.IAS = (float)AV.indicatedAirSpeed;
VP.CurrentStage = (byte)StageManager.CurrentStage;
VP.TotalStage = (byte)StageManager.StageCount;
VP.SpeedMode = (byte)(FlightGlobals.speedDisplayMode + 1);
VP.SASMode = GetSASMode(true);
VP.timeWarpRateIndex = GetTimeWarpIndex();
}
public Vector3 GetFwdVector()
{
return(target == null? Vector3.up : target.GetFwdVector());
}
