Exemplo n.º 1
0
        public static double GetProtonRadiationLevel(this CelestialBody body, CelestialBody homeworld, double altitude, double lat)
        {
            lat = lat / 180 * Math.PI;

            double atmosphere    = FlightGlobals.getStaticPressure(altitude, body) / 101.325;
            double relrp         = body.Radius / homeworld.Radius;
            double relrt         = body.rotationPeriod / homeworld.rotationPeriod;
            double peakbelt      = body.GetPeakProtonBeltAltitude(homeworld, altitude, lat);
            double altituded     = altitude;
            double a             = peakbelt / sqrt2;
            double beltparticles = sqrt2divPi * Math.Pow(altituded, 2) * Math.Exp(-Math.Pow(altituded, 2) / (2 * Math.Pow(a, 2))) / (Math.Pow(a, 3));

            beltparticles = beltparticles * relrp / relrt * 50;

            if (KopernicusHelper.IsStar(body))
            {
                beltparticles /= 1000;
            }

            if (body.atmosphere)
            {
                beltparticles *= body.atmosphereDepth / 70000;
            }
            else
            {
                beltparticles *= 0.01;
            }

            beltparticles = beltparticles * Math.Abs(Math.Cos(lat)) * body.specialMagneticFieldScaling() * Math.Exp(-atmosphere);

            return(beltparticles);
        }
        public override void OnUpdate()
        {
            base.OnUpdate();

            vesselAltitudeInKm = vessel.altitude * 0.001;
            inStarOrbit        = KopernicusHelper.IsStar(vessel.mainBody);
        }
Exemplo n.º 3
0
        public static double getBeltMagneticFieldAzimuthal(this CelestialBody body, CelestialBody homeworld, double altitude, double lat)
        {
            double mlat = lat / 180 * Math.PI + Math.PI / 2;

            double relmp = body.Mass / homeworld.Mass;
            double relrp = body.Radius / homeworld.Radius;
            double relrt = body.rotationPeriod / homeworld.rotationPeriod;

            double altituded = altitude + body.Radius;
            double Bmag      = -relmp * VanAllen.B0 / relrt * Math.Pow((body.Radius / altituded), 3) * Math.Sin(mlat) * body.specialMagneticFieldScaling();

            if (KopernicusHelper.IsStar(body))
            {
                Bmag /= 1000;
            }

            if (body.atmosphere)
            {
                Bmag *= body.atmosphereDepth / 70000;
            }
            else
            {
                Bmag *= 0.01;
            }

            return(Bmag);
        }
Exemplo n.º 4
0
        public static double GetElectronRadiationLevel(this CelestialBody body, CelestialBody homeworld, double altitude, double lat)
        {
            lat = lat / 180 * Math.PI;
            double atmosphere         = FlightGlobals.getStaticPressure(altitude, body) / GameConstants.EarthAtmospherePressureAtSeaLevel;
            double atmosphere_height  = PluginHelper.GetMaxAtmosphericAltitude(body);
            double atmosphere_scaling = Math.Exp(-atmosphere);

            double relrp = body.Radius / homeworld.Radius;
            double relrt = body.rotationPeriod / homeworld.rotationPeriod;

            double peakbelt2     = body.GetPeakElectronBeltAltitude(homeworld, altitude, lat);
            double altituded     = altitude;
            double b             = peakbelt2 / sqrt2;
            double beltparticles = 0.9 * sqrt2divPi * Math.Pow(altituded, 2) * Math.Exp(-Math.Pow(altituded, 2) / (2 * Math.Pow(b, 2))) / (Math.Pow(b, 3));

            beltparticles = beltparticles * relrp / relrt * 50;

            if (KopernicusHelper.IsStar(body))
            {
                beltparticles /= 1000;
            }

            if (body.atmosphere)
            {
                beltparticles *= body.atmosphereDepth / 70000;
            }
            else
            {
                beltparticles *= 0.01;
            }

            beltparticles = beltparticles * Math.Abs(Math.Cos(lat)) * body.specialMagneticFieldScaling() * atmosphere_scaling;

            return(beltparticles);
        }
        public static double GetBeltMagneticFieldRadial(this CelestialBody body, CelestialBody homeworld, double altitude, double lat)
        {
            double mlat = lat / 180 * Math.PI + Math.PI / 2;

            double relmp = body.Mass / homeworld.Mass;
            double relrt = body.rotationPeriod / homeworld.rotationPeriod;

            double altituded = altitude + body.Radius;
            double Bmag      = -2 / relrt * relmp * VanAllen.B0 * Math.Pow((body.Radius / altituded), 3) * Math.Cos(mlat) * body.SpecialMagneticFieldScaling();

            if (KopernicusHelper.GetLuminocity(body) > 0)
            {
                Bmag /= 1000;
            }

            if (body.atmosphere)
            {
                Bmag *= body.atmosphereDepth / 70000;
            }
            else
            {
                Bmag *= 0.01;
            }

            return(Bmag);
        }
Exemplo n.º 6
0
        private static void ProcessUnloadedSolarPanels(VesselData vesselData)
        {
            if (DetectKerbalism.Found)
            {
                return;
            }

            if (!vesselData.SolarPanels.Any())
            {
                return;
            }

            foreach (StarLight starlight in KopernicusHelper.Stars)
            {
                double starlightRelativeLuminosity = KopernicusHelper.GetSolarDistanceMultiplier(
                    vesselPosition: vesselData.Position,
                    star: starlight.star,
                    astronomicalUnit: KopernicusHelper.AstronomicalUnit);

                starlightRelativeLuminosity *= starlight.relativeLuminosity;

                // ignore stars that are too far away to give any meaningful energy
                if (starlightRelativeLuminosity < 0.001)
                {
                    continue;
                }

                // ignore if there is no line of sight between the star and the vessel
                if (!KopernicusHelper.LineOfSightToSun(vesselData.Position, starlight.star))
                {
                    continue;
                }

                foreach (KeyValuePair <uint, SolarPanelData> keyValuePair in vesselData.SolarPanels)
                {
                    SolarPanelData solarPanelData = keyValuePair.Value;

                    foreach (ModuleDeployableSolarPanel solarPanel in solarPanelData.ModuleDeployableSolarPanels)
                    {
                        if (solarPanel.chargeRate <= 0)
                        {
                            continue;
                        }

                        if (solarPanel.deployState != ModuleDeployablePart.DeployState.EXTENDED)
                        {
                            continue;
                        }

                        double trackingModifier = solarPanel.isTracking ? 1 : 0.25;
                        double powerChange      = trackingModifier * solarPanel.chargeRate * starlightRelativeLuminosity * solarPanel.efficiencyMult * solarPanelData.ChargeRateMultiplier;

                        vesselData.UpdateAvailableResource(solarPanel.resourceName, powerChange);
                        vesselData.ResourceChange(solarPanel.resourceName, powerChange);
                    }
                }
            }
        }
Exemplo n.º 7
0
        public static double GetBeltAntiparticles(this CelestialBody body, CelestialBody homeworld, double altitude, double lat)
        {
            if (body.flightGlobalsIndex != 0 && altitude <= PluginHelper.getMaxAtmosphericAltitude(body))
            {
                return(0);
            }

            BeltData beltdata;

            if (!BeltDataCache.TryGetValue(body.name, out beltdata))
            {
                double relrp = body.Radius / homeworld.Radius;
                double relrt = body.rotationPeriod / homeworld.rotationPeriod;

                beltdata = new BeltData()
                {
                    density = body.Mass / homeworld.Mass * relrp / relrt * 50,
                    ampere  = 1.5 * homeworld.Radius * relrp / sqrt2,
                };

                BeltDataCache.Add(body.name, beltdata);
            }

            double beltparticles = beltdata.density
                                   * sqrt2divPi
                                   * Math.Pow(altitude, 2)
                                   * Math.Exp(-Math.Pow(altitude, 2) / (2 * Math.Pow(beltdata.ampere, 2)))
                                   / (Math.Pow(beltdata.ampere, 3));

            if (KopernicusHelper.GetLuminocity(body) > 0)
            {
                beltparticles /= 1000;
            }

            if (body.atmosphere)
            {
                beltparticles *= body.atmosphereDepth / 70000;
            }
            else
            {
                beltparticles *= 0.01;
            }

            return(beltparticles * Math.Abs(Math.Cos(lat / 180 * Math.PI)) * body.specialMagneticFieldScaling());
        }