示例#1
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 public override void FixedUpdate(TimeStep timeStep)
 {
     if (Parent == null)
     {
         OrbitHelper.TraceSpaceCraft(this, OrbitTrace);
     }
 }
示例#2
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    Vector3 VectorForUnity(DataRow row)
    {
        Vector3Double vec = OrbitHelper.OrbitalStateVectors(GetDouble(row[2]), GetDouble(row[3]), GetDouble(row[4]), GetDouble(row[5]), GetDouble(row[6]), GetDouble(row[8]));//Calculations.CalculateOrbitalPosition(GetDouble(row[2]), GetDouble(row[3]), GetDouble(row[4]), GetDouble(row[5]), GetDouble(row[6]), GetDouble(row[8]));

        Vector3 v = (vec / div).ToFLoat();

        return(v);
    }
示例#3
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 public Europa(DVector2 parentPositon, DVector2 parentVelocity)
     : base(OrbitHelper.FromJplEphemeris(6.156481591252791E+05, 2.501017249378511E+05) + parentPositon,
            OrbitHelper.FromJplEphemeris(-5.263255140302287E+00, 1.282255171501272E+01) + parentVelocity, new EuropaKernel())
 {
 }
示例#4
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 public Saturn()
     : base(OrbitHelper.FromJplEphemeris(-3.667006922888632E+08, -1.455132410758398E+09),
            OrbitHelper.FromJplEphemeris(8.836135826121589E+00, -2.389892378353466E+00), new SaturnKernel())
 {
 }
示例#5
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 public Venus()
     : base(OrbitHelper.FromJplEphemeris(-7.107549422541827E+07, -8.069630266378376E+07),
            OrbitHelper.FromJplEphemeris(2.601196797328043E+01, -2.332263510301460E+01), new VenusKernel())
 {
 }
示例#6
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文件: Sun.cs 项目: stauders/SpaceSim
 public Sun()
     : base(OrbitHelper.FromJplEphemeris(5.432947986595253E+05, 4.730052562792657E+05),
            OrbitHelper.FromJplEphemeris(-2.899962878525558E-03, 1.198996655704255E-02), new SunKernel())
 {
 }
示例#7
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 public Saturn()
     : base(OrbitHelper.GetPosition(1.3526e12, 1.6132416870058, DVector2.Zero),
            OrbitHelper.GetVelocity(1.3526e12, 1.6132416870058, -1.018e4, DVector2.Zero), new SaturnKernel())
 {
 }
示例#8
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 public Earth(double inclination)
     : base(OrbitHelper.FromJplEphemeris(1.470669705624798E+08, -3.465263667484938E+07),
            OrbitHelper.FromJplEphemeris(6.445708901348731E+00, 2.887242866160539E+01), new EarthKernel())
 {
     this.inclination = Math.Cos(inclination * MathHelper.DegreesToRadians);;
 }
示例#9
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 public Jupiter()
     : base(OrbitHelper.GetPosition(7.405736e11, 0.25750325984, DVector2.Zero),
            OrbitHelper.GetVelocity(7.405736e11, 0.25750325984, -1.372e4, DVector2.Zero), new JupiterKernel())
 {
 }
示例#10
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 public Mercury()
     : base(OrbitHelper.FromJplEphemeris(5.246226302537809E+07, -2.527033713925028E+07),
            OrbitHelper.FromJplEphemeris(1.211166887870701E+01, 4.586947862338018E+01), new MercuryKernel())
 {
 }
示例#11
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 public Moon(DVector2 positionOffset, DVector2 velocityOffset)
     : base(OrbitHelper.GetPosition(3.63295e8, 0.2967059, positionOffset),
            OrbitHelper.GetVelocity(3.63295e8, 0.2967059, -1076.0, velocityOffset), new MoonKernel())
 {
 }
示例#12
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 public Mars()
     : base(OrbitHelper.FromJplEphemeris(1.186183757284019E+08, -1.722428244606592E+08),
            OrbitHelper.FromJplEphemeris(2.091501229864822E+01, 1.576687031430872E+01), new MarsKernel())
 {
 }
示例#13
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文件: Venus.cs 项目: rdancer/SpaceSim
 public Venus()
     : base(OrbitHelper.GetPosition(1.07477e11, 2.29568357, DVector2.Zero),
            OrbitHelper.GetVelocity(1.07477e11, 2.29568357, -3.526e4, DVector2.Zero), new VenusKernel())
 {
 }
示例#14
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 public Mercury()
     : base(OrbitHelper.GetPosition(4.6001200e10, 1.35187, DVector2.Zero),
            OrbitHelper.GetVelocity(4.6001200e10, 1.35187, -5.898e4, DVector2.Zero), new MercuryKernel())
 {
 }
示例#15
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 public Earth()
     : base(OrbitHelper.GetPosition(1.47095e11, 1.7967674211, DVector2.Zero),
            OrbitHelper.GetVelocity(1.47095e11, 1.7967674211, -3.029e4, DVector2.Zero), new EarthKernel())
 {
 }
示例#16
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 public Ganymede(DVector2 parentPositon, DVector2 parentVelocity)
     : base(OrbitHelper.FromJplEphemeris(-9.194475286771294E+05, -5.471806593872152E+05) + parentPositon,
            OrbitHelper.FromJplEphemeris(5.585068938118295E+00, -9.333406535151921E+00) + parentVelocity, new GanymedeKernel())
 {
 }
示例#17
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 public Jupiter()
     : base(OrbitHelper.FromJplEphemeris(-8.140496172394816E+08, -2.921133413936896E+07),
            OrbitHelper.FromJplEphemeris(3.165828961330318E-01, -1.243819908039714E+01), new JupiterKernel())
 {
 }
示例#18
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 public Moon(DVector2 parentPositon, DVector2 parentVelocity)
     : base(OrbitHelper.FromJplEphemeris(-1.275488485528684E+05, -3.756609087364946E+05) + parentPositon,
            OrbitHelper.FromJplEphemeris(9.291844409239249E-01, -2.857101216046916E-01) + parentVelocity, new MoonKernel())
 {
 }
示例#19
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 public Mars()
     : base(OrbitHelper.GetPosition(2.067e11, 5.865019079167, DVector2.Zero),
            OrbitHelper.GetVelocity(2.067e11, 5.865019079167, -2.65e4, DVector2.Zero), new MarsKernel())
 {
 }
示例#20
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 public override void FixedUpdate(TimeStep timeStep)
 {
     OrbitHelper.TraceMassiveBody(this, OrbitTrace);
 }
示例#21
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 public Callisto(DVector2 parentPositon, DVector2 parentVelocity)
     : base(OrbitHelper.FromJplEphemeris(-1.838974425381978E+06, 4.612334321076249E+05) + parentPositon,
            OrbitHelper.FromJplEphemeris(-1.996468410126901E+00, -7.894863713236139E+00) + parentVelocity, new CallistoKernel())
 {
 }
示例#22
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 public Earth()
     : base(OrbitHelper.FromJplEphemeris(1.470669705624798E+08, -3.465263667484938E+07),
            OrbitHelper.FromJplEphemeris(6.445708901348731E+00, 2.887242866160539E+01), new EarthKernel())
 {
 }
示例#23
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文件: Io.cs 项目: stauders/SpaceSim
 public Io(DVector2 parentPositon, DVector2 parentVelocity)
     : base(OrbitHelper.FromJplEphemeris(-4.187887882620349E+05, -3.532782596227979E+04) + parentPositon,
            OrbitHelper.FromJplEphemeris(1.513295262903566E+00, -1.731988564333744E+01) + parentVelocity, new IoKernel())
 {
 }