コード例 #1
0
        /// <summary>
        /// Get ressource information by ressource name.
        /// Name can be
        ///  - XenonGas
        ///  - SolidFuel
        ///  - IntakeAir
        ///  - MonoPropellant
        ///  - ElectricCharge
        ///  - Oxidizer
        ///  - LiquidFuel
        ///
        /// </summary>
        /// <param name="V">Vessel</param>
        /// <param name="resourceName">Name of the ressource</param>
        /// <returns>Max and actual amount</returns>
        private IOResource GetResourceTotal(Vessel V, string resourceName)
        {
            IOResource R = new IOResource();

            foreach (Part p in V.parts)
            {
                foreach (PartResource pr in p.Resources)
                {
                    if (pr.resourceName.Equals(resourceName))
                    {
                        R.Current += (float)pr.amount;
                        R.Max     += (float)pr.maxAmount;

                        break;
                    }
                }
            }

            if (R.Max == 0)
            {
                R.Current = 0;
            }

            return(R);
        }
コード例 #2
0
        public void Awake()
        {
            TempR = new IOResource();
            DontDestroyOnLoad(gameObject);
            msg("Starting YARK KSPWebsockIO");

            SP             = new StatusPacket();
            SP.YarkVersion = YARK_VERSION;
            VP             = new VesselPacket();

            server = new TcpListener(IPAddress.Any, Config.TCPPort);
            server.Start();

            inFlight = -1;
        }
コード例 #3
0
 public DeployedResourceAttribute(string resource)
 {
     Resource = IOResource.From(resource);
 }
コード例 #4
0
        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();
        }
コード例 #5
0
        /// <summary>
        /// Runs a timer. If the refresh time is exceed updates all vessel data and
        /// triggers a VesselDataInvalidated event.
        /// </summary>
        public void UpdateVesselData()
        {
            if (FlightGlobals.ActiveVessel != null)
            {
                bool vesselChanged = false;
                if (_activeVessel == null || _activeVessel.id != FlightGlobals.ActiveVessel.id)
                {
                    vesselChanged = true;
                }
                if (vesselChanged)
                {
                    _activeVessel = FlightGlobals.ActiveVessel;
                    _vData.vesselSync++;
                    if (_vData.vesselSync == 0)
                    {
                        _vData.vesselSync++;
                    }
                    _vesselSync = _vData.vesselSync;
                }

                _theTime = Time.unscaledTime;
                if ((_theTime - _lastUpdate) * 1000 > _refreshrate)
                {
                    IOResource TempR = new IOResource();

                    Vessel ActiveVessel = FlightGlobals.ActiveVessel;

                    _lastUpdate = _theTime;

                    List <Part> ActiveEngines = new List <Part>();
                    ActiveEngines = GetListOfActivatedEngines(ActiveVessel);

                    _vData.AP            = (float)ActiveVessel.orbit.ApA;
                    _vData.PE            = (float)ActiveVessel.orbit.PeA;
                    _vData.SemiMajorAxis = (float)ActiveVessel.orbit.semiMajorAxis;
                    _vData.SemiMinorAxis = (float)ActiveVessel.orbit.semiMinorAxis;
                    _vData.e             = (float)ActiveVessel.orbit.eccentricity;
                    _vData.inc           = (float)ActiveVessel.orbit.inclination;
                    _vData.VVI           = (float)ActiveVessel.verticalSpeed;
                    _vData.G             = (float)ActiveVessel.geeForce;
                    _vData.TAp           = (int)Math.Round(ActiveVessel.orbit.timeToAp);
                    _vData.TPe           = (int)Math.Round(ActiveVessel.orbit.timeToPe);
                    _vData.Density       = (float)ActiveVessel.atmDensity;
                    _vData.TrueAnomaly   = (float)ActiveVessel.orbit.trueAnomaly;
                    _vData.period        = (int)Math.Round(ActiveVessel.orbit.period);

                    double ASL = ActiveVessel.mainBody.GetAltitude(ActiveVessel.CoM);
                    double AGL = (ASL - ActiveVessel.terrainAltitude);

                    if (AGL < ASL)
                    {
                        _vData.RAlt = (float)AGL;
                    }
                    else
                    {
                        _vData.RAlt = (float)ASL;
                    }

                    _vData.Alt   = (float)ASL;
                    _vData.Vsurf = (float)ActiveVessel.srfSpeed;
                    _vData.Lat   = (float)ActiveVessel.latitude;
                    _vData.Lon   = (float)ActiveVessel.longitude;

                    TempR = GetResourceTotal(ActiveVessel, "LiquidFuel");
                    _vData.LiquidFuelTot = TempR.Max;
                    _vData.LiquidFuel    = TempR.Current;

                    _vData.LiquidFuelTotS = (float)ProspectForResourceMax("LiquidFuel", ActiveEngines);
                    _vData.LiquidFuelS    = (float)ProspectForResource("LiquidFuel", ActiveEngines);

                    TempR = GetResourceTotal(ActiveVessel, "Oxidizer");
                    _vData.OxidizerTot = TempR.Max;
                    _vData.Oxidizer    = TempR.Current;

                    _vData.OxidizerTotS = (float)ProspectForResourceMax("Oxidizer", ActiveEngines);
                    _vData.OxidizerS    = (float)ProspectForResource("Oxidizer", ActiveEngines);

                    TempR               = GetResourceTotal(ActiveVessel, "ElectricCharge");
                    _vData.EChargeTot   = TempR.Max;
                    _vData.ECharge      = TempR.Current;
                    TempR               = GetResourceTotal(ActiveVessel, "MonoPropellant");
                    _vData.MonoPropTot  = TempR.Max;
                    _vData.MonoProp     = TempR.Current;
                    TempR               = GetResourceTotal(ActiveVessel, "IntakeAir");
                    _vData.IntakeAirTot = TempR.Max;
                    _vData.IntakeAir    = TempR.Current;
                    TempR               = GetResourceTotal(ActiveVessel, "SolidFuel");
                    _vData.SolidFuelTot = TempR.Max;
                    _vData.SolidFuel    = TempR.Current;
                    TempR               = GetResourceTotal(ActiveVessel, "XenonGas");
                    _vData.XenonGasTot  = TempR.Max;
                    _vData.XenonGas     = TempR.Current;

                    _missionTime    = ActiveVessel.missionTime;
                    _deltaT         = _missionTime - _missionTimeOld;
                    _missionTimeOld = _missionTime;

                    _vData.MissionTime = (UInt32)Math.Round(_missionTime);
                    _vData.deltaTime   = (float)_deltaT;

                    _vData.VOrbit = (float)ActiveVessel.orbit.GetVel().magnitude;

                    Vector3d   CoM, north, up, east;
                    Quaternion rotationSurface;
                    CoM             = ActiveVessel.CoM;
                    up              = (CoM - ActiveVessel.mainBody.position).normalized;
                    north           = Vector3d.Exclude(up, (ActiveVessel.mainBody.position + ActiveVessel.mainBody.transform.up * (float)ActiveVessel.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(ActiveVessel.GetTransform().rotation) * rotationSurface).eulerAngles;

                    _vData.Roll    = ToScaledUInt((attitude.z > 180) ? (attitude.z - 360.0) : attitude.z);
                    _vData.Pitch   = ToScaledUInt((attitude.x > 180) ? (attitude.x - 360.0) : attitude.x);
                    _vData.Heading = ToScaledUInt((attitude.y > 180) ? (attitude.y - 360.0) : attitude.y);

                    Vector3d prograde = new Vector3d(0, 0, 0);
                    switch (FlightGlobals.speedDisplayMode)
                    {
                    case FlightGlobals.SpeedDisplayModes.Surface:
                        prograde = ActiveVessel.srf_velocity.normalized;
                        break;

                    case FlightGlobals.SpeedDisplayModes.Orbit:
                        prograde = ActiveVessel.obt_velocity.normalized;
                        break;

                    case FlightGlobals.SpeedDisplayModes.Target:
                        prograde = FlightGlobals.ship_tgtVelocity;
                        break;
                    }

                    NavHeading zeroHeading; zeroHeading.Pitch = zeroHeading.Heading = 0;
                    NavHeading Prograde = WorldVecToNavHeading(up, north, east, prograde), Target = zeroHeading, Maneuver = zeroHeading;

                    _vData.ProgradeHeading = ToScaledUInt(Prograde.Heading);
                    _vData.ProgradePitch   = ToScaledUInt(Prograde.Pitch);

                    if (TargetExists())
                    {
                        _vData.TargetDist = (float)Vector3.Distance(FlightGlobals.fetch.VesselTarget.GetVessel().transform.position, ActiveVessel.transform.position);
                        _vData.TargetV    = (float)FlightGlobals.ship_tgtVelocity.magnitude;
                        Target            = WorldVecToNavHeading(up, north, east, ActiveVessel.targetObject.GetTransform().position - ActiveVessel.transform.position);
                    }
                    _vData.TargetHeading = ToScaledUInt(Target.Heading);
                    _vData.TargetPitch   = ToScaledUInt(Target.Pitch);

                    _vData.NormalHeading = ToScaledUInt(WorldVecToNavHeading(up, north, east, Vector3d.Cross(ActiveVessel.obt_velocity.normalized, up)).Heading);


                    _vData.MNTime   = 0;
                    _vData.MNDeltaV = 0;
                    if (ActiveVessel.patchedConicSolver != null)
                    {
                        if (ActiveVessel.patchedConicSolver.maneuverNodes != null)
                        {
                            if (ActiveVessel.patchedConicSolver.maneuverNodes.Count > 0)
                            {
                                _vData.MNTime   = (UInt32)Math.Round(ActiveVessel.patchedConicSolver.maneuverNodes[0].UT - Planetarium.GetUniversalTime());
                                _vData.MNDeltaV = (float)ActiveVessel.patchedConicSolver.maneuverNodes[0].GetBurnVector(ActiveVessel.patchedConicSolver.maneuverNodes[0].patch).magnitude; //Added JS

                                Maneuver = WorldVecToNavHeading(up, north, east, ActiveVessel.patchedConicSolver.maneuverNodes[0].GetBurnVector(ActiveVessel.patchedConicSolver.maneuverNodes[0].patch));
                            }
                        }
                    }
                    _vData.ManeuverHeading = ToScaledUInt(Maneuver.Heading);
                    _vData.ManeuverPitch   = ToScaledUInt(Maneuver.Pitch);



                    ControlStatus((int)EnumAG.SAS, ActiveVessel.ActionGroups[KSPActionGroup.SAS]);
                    ControlStatus((int)EnumAG.RCS, ActiveVessel.ActionGroups[KSPActionGroup.RCS]);
                    ControlStatus((int)EnumAG.Light, ActiveVessel.ActionGroups[KSPActionGroup.Light]);
                    ControlStatus((int)EnumAG.Gear, ActiveVessel.ActionGroups[KSPActionGroup.Gear]);
                    ControlStatus((int)EnumAG.Brakes, ActiveVessel.ActionGroups[KSPActionGroup.Brakes]);
                    ControlStatus((int)EnumAG.Abort, ActiveVessel.ActionGroups[KSPActionGroup.Abort]);
                    ControlStatus((int)EnumAG.Custom01, ActiveVessel.ActionGroups[KSPActionGroup.Custom01]);
                    ControlStatus((int)EnumAG.Custom02, ActiveVessel.ActionGroups[KSPActionGroup.Custom02]);
                    ControlStatus((int)EnumAG.Custom03, ActiveVessel.ActionGroups[KSPActionGroup.Custom03]);
                    ControlStatus((int)EnumAG.Custom04, ActiveVessel.ActionGroups[KSPActionGroup.Custom04]);
                    ControlStatus((int)EnumAG.Custom05, ActiveVessel.ActionGroups[KSPActionGroup.Custom05]);
                    ControlStatus((int)EnumAG.Custom06, ActiveVessel.ActionGroups[KSPActionGroup.Custom06]);
                    ControlStatus((int)EnumAG.Custom07, ActiveVessel.ActionGroups[KSPActionGroup.Custom07]);
                    ControlStatus((int)EnumAG.Custom08, ActiveVessel.ActionGroups[KSPActionGroup.Custom08]);
                    ControlStatus((int)EnumAG.Custom09, ActiveVessel.ActionGroups[KSPActionGroup.Custom09]);
                    ControlStatus((int)EnumAG.Custom10, ActiveVessel.ActionGroups[KSPActionGroup.Custom10]);

                    if (ActiveVessel.orbit.referenceBody != null)
                    {
                        _vData.SOINumber = GetSOINumber(ActiveVessel.orbit.referenceBody.name);
                    }

                    _vData.MaxOverHeat  = GetMaxOverHeat(ActiveVessel);
                    _vData.MachNumber   = (float)ActiveVessel.mach;
                    _vData.IAS          = (float)ActiveVessel.indicatedAirSpeed;
                    _vData.CurrentStage = (byte)StageManager.CurrentStage;
                    _vData.TotalStage   = (byte)StageManager.StageCount;

                    _vData.NavballSASMode = (byte)(((int)FlightGlobals.speedDisplayMode + 1) << 4); //get navball speed display mode
                    if (ActiveVessel.ActionGroups[KSPActionGroup.SAS])
                    {
                        _vData.NavballSASMode = (byte)(((int)FlightGlobals.ActiveVessel.Autopilot.Mode + 1) | _vData.NavballSASMode);
                    }


                    //target distance and velocity stuff

                    _vData.TargetDist = 0;
                    _vData.TargetV    = 0;

                    if (TargetExists())
                    {
                        _vData.TargetDist = (float)Vector3.Distance(FlightGlobals.fetch.VesselTarget.GetVessel().transform.position, ActiveVessel.transform.position);
                        _vData.TargetV    = (float)FlightGlobals.ship_tgtVelocity.magnitude;
                    }


                    _vData.NavballSASMode = (byte)(((int)FlightGlobals.speedDisplayMode + 1) << 4); //get navball speed display mode
                    if (ActiveVessel.ActionGroups[KSPActionGroup.SAS])
                    {
                        _vData.NavballSASMode = (byte)(((int)FlightGlobals.ActiveVessel.Autopilot.Mode + 1) | _vData.NavballSASMode);
                    }


                    //Notify listeners
                    NotifyInvalidate(_vData);
                }
            }
        }