%General Mission Analysis Tool(GMAT) Script
%Created: 2018-04-08 22:17:07
%----------------------------------------
%---------- Spacecraft
%----------------------------------------
Create Spacecraft FromCart;
GMAT FromCart.DateFormat = TAIModJulian;
GMAT FromCart.Epoch = '21545';
GMAT FromCart.CoordinateSystem = EarthMJ2000Eq;
GMAT FromCart.DisplayStateType = Cartesian;
GMAT FromCart.X = 5946.673548288958;
GMAT FromCart.Y = 1656.154606023661;
GMAT FromCart.Z = 2259.012129598249;
GMAT FromCart.VX = -3.098683050943824;
GMAT FromCart.VY = 4.579534132135011;
GMAT FromCart.VZ = 6.246541551539432;
GMAT FromCart.DryMass = 850;
GMAT FromCart.Cd = 2.2;
GMAT FromCart.Cr = 1.8;
GMAT FromCart.DragArea = 15;
GMAT FromCart.SRPArea = 1;
GMAT FromCart.NAIFId = -10000001;
GMAT FromCart.NAIFIdReferenceFrame = -9000001;
GMAT FromCart.OrbitColor = Red;
GMAT FromCart.TargetColor = Teal;
GMAT FromCart.EstimationStateType = 'Cartesian';
GMAT FromCart.OrbitErrorCovariance = [ 1e+70 0 0 0 0 0 ; 0 1e+70 0 0 0 0 ; 0 0 1e+70 0 0 0 ; 0 0 0 1e+70 0 0 ; 0 0 0 0 1e+70 0 ; 0 0 0 0 0 1e+70 ];
GMAT FromCart.CdSigma = 1e+70;
GMAT FromCart.CrSigma = 1e+70;
GMAT FromCart.Id = 'SatId';
GMAT FromCart.Attitude = CoordinateSystemFixed;
GMAT FromCart.SPADSRPScaleFactor = 1;
GMAT FromCart.ModelFile = 'aura.3ds';
GMAT FromCart.ModelOffsetX = 0;
GMAT FromCart.ModelOffsetY = 0;
GMAT FromCart.ModelOffsetZ = 0;
GMAT FromCart.ModelRotationX = 0;
GMAT FromCart.ModelRotationY = 0;
GMAT FromCart.ModelRotationZ = 0;
GMAT FromCart.ModelScale = 1;
GMAT FromCart.AttitudeDisplayStateType = 'Quaternion';
GMAT FromCart.AttitudeRateDisplayStateType = 'AngularVelocity';
GMAT FromCart.AttitudeCoordinateSystem = EarthMJ2000Eq;
GMAT FromCart.EulerAngleSequence = '321';
Create Spacecraft FromKep;
GMAT FromKep.DateFormat = TAIModJulian;
GMAT FromKep.Epoch = '21545';
GMAT FromKep.CoordinateSystem = EarthMJ2000Eq;
GMAT FromKep.DisplayStateType = Keplerian;
GMAT FromKep.SMA = 8191.930000000003;
GMAT FromKep.ECC = 0.02450000000000035;
GMAT FromKep.INC = 12.85000000000002;
GMAT FromKep.RAAN = 306.614;
GMAT FromKep.AOP = 314.1900000000004;
GMAT FromKep.TA = 99.88769999999958;
GMAT FromKep.DryMass = 850;
GMAT FromKep.Cd = 2.2;
GMAT FromKep.Cr = 1.8;
GMAT FromKep.DragArea = 15;
GMAT FromKep.SRPArea = 1;
GMAT FromKep.NAIFId = -10002001;
GMAT FromKep.NAIFIdReferenceFrame = -9002001;
GMAT FromKep.OrbitColor = Green;
GMAT FromKep.TargetColor = LightGray;
GMAT FromKep.EstimationStateType = 'Cartesian';
GMAT FromKep.OrbitErrorCovariance = [ 1e+70 0 0 0 0 0 ; 0 1e+70 0 0 0 0 ; 0 0 1e+70 0 0 0 ; 0 0 0 1e+70 0 0 ; 0 0 0 0 1e+70 0 ; 0 0 0 0 0 1e+70 ];
GMAT FromKep.CdSigma = 1e+70;
GMAT FromKep.CrSigma = 1e+70;
GMAT FromKep.Id = 'SatId';
GMAT FromKep.Attitude = CoordinateSystemFixed;
GMAT FromKep.SPADSRPScaleFactor = 1;
GMAT FromKep.ModelFile = 'aura.3ds';
GMAT FromKep.ModelOffsetX = 0;
GMAT FromKep.ModelOffsetY = 0;
GMAT FromKep.ModelOffsetZ = 0;
GMAT FromKep.ModelRotationX = 0;
GMAT FromKep.ModelRotationY = 0;
GMAT FromKep.ModelRotationZ = 0;
GMAT FromKep.ModelScale = 1;
GMAT FromKep.AttitudeDisplayStateType = 'Quaternion';
GMAT FromKep.AttitudeRateDisplayStateType = 'AngularVelocity';
GMAT FromKep.AttitudeCoordinateSystem = EarthMJ2000Eq;
GMAT FromKep.EulerAngleSequence = '321';
%----------------------------------------
%---------- ForceModels
%----------------------------------------
Create ForceModel DefaultProp_ForceModel;
GMAT DefaultProp_ForceModel.CentralBody = Earth;
GMAT DefaultProp_ForceModel.PointMasses = {Earth};
GMAT DefaultProp_ForceModel.Drag = None;
GMAT DefaultProp_ForceModel.SRP = Off;
GMAT DefaultProp_ForceModel.RelativisticCorrection = Off;
GMAT DefaultProp_ForceModel.ErrorControl = RSSState;
%----------------------------------------
%---------- Propagators
%----------------------------------------
Create Propagator DefaultProp;
GMAT DefaultProp.FM = DefaultProp_ForceModel;
GMAT DefaultProp.Type = RungeKutta89;
GMAT DefaultProp.InitialStepSize = 30;
GMAT DefaultProp.Accuracy = 1e-12;
GMAT DefaultProp.MinStep = 0.1;
GMAT DefaultProp.MaxStep = 30;
GMAT DefaultProp.MaxStepAttempts = 50;
GMAT DefaultProp.StopIfAccuracyIsViolated = true;
%----------------------------------------
%---------- Subscribers
%----------------------------------------
Create ReportFile ReportFromCart;
GMAT ReportFromCart.SolverIterations = Current;
GMAT ReportFromCart.UpperLeft = [ 0.1458333333333333 0.03414634146341464 ];
GMAT ReportFromCart.Size = [ 0.9940476190476191 0.9634146341463414 ];
GMAT ReportFromCart.RelativeZOrder = 1;
GMAT ReportFromCart.Maximized = true;
GMAT ReportFromCart.Filename = 'ReportFromCart.txt';
GMAT ReportFromCart.Precision = 16;
GMAT ReportFromCart.Add = {FromCart.EarthMJ2000Eq.HX, FromCart.EarthMJ2000Eq.HY, FromCart.EarthMJ2000Eq.HZ, FromCart.Earth.Energy, FromCart.Earth.OrbitPeriod, FromCart.Earth.SMA, FromCart.Earth.ECC, FromCart.EarthMJ2000Eq.INC, FromCart.EarthMJ2000Eq.RAAN, FromCart.EarthMJ2000Eq.AOP, FromCart.Earth.TA, FromCart.EarthMJ2000Eq.TLONG, FromCart.Earth.EA, FromCart.Earth.MA, FromCart.Earth.RadApo, FromCart.Earth.RadPer, FromCart.Earth.SemilatusRectum};
GMAT ReportFromCart.WriteHeaders = true;
GMAT ReportFromCart.LeftJustify = On;
GMAT ReportFromCart.ZeroFill = Off;
GMAT ReportFromCart.FixedWidth = true;
GMAT ReportFromCart.Delimiter = ' ';
GMAT ReportFromCart.ColumnWidth = 23;
GMAT ReportFromCart.WriteReport = true;
Create ReportFile ReportFromKep;
GMAT ReportFromKep.SolverIterations = Current;
GMAT ReportFromKep.UpperLeft = [ 0.1458333333333333 0.03414634146341464 ];
GMAT ReportFromKep.Size = [ 0.9940476190476191 0.9634146341463414 ];
GMAT ReportFromKep.RelativeZOrder = 1;
GMAT ReportFromKep.Maximized = true;
GMAT ReportFromKep.Filename = 'ReportFromKep.txt';
GMAT ReportFromKep.Precision = 16;
GMAT ReportFromKep.Add = {FromKep.EarthMJ2000Eq.X, FromKep.EarthMJ2000Eq.Y, FromKep.EarthMJ2000Eq.Z, FromKep.EarthMJ2000Eq.VX, FromKep.EarthMJ2000Eq.VY, FromKep.EarthMJ2000Eq.VZ, FromKep.EarthMJ2000Eq.HX, FromKep.EarthMJ2000Eq.HY, FromKep.EarthMJ2000Eq.HZ, FromKep.Earth.Energy, FromKep.Earth.OrbitPeriod, FromKep.Earth.SMA, FromKep.Earth.ECC, FromKep.EarthMJ2000Eq.INC, FromKep.EarthMJ2000Eq.RAAN, FromKep.EarthMJ2000Eq.AOP, FromKep.Earth.TA, FromKep.EarthMJ2000Eq.TLONG, FromKep.Earth.EA, FromKep.Earth.MA, FromKep.Earth.RadApo, FromKep.Earth.RadPer, FromKep.Earth.SemilatusRectum};
GMAT ReportFromKep.WriteHeaders = true;
GMAT ReportFromKep.LeftJustify = On;
GMAT ReportFromKep.ZeroFill = Off;
GMAT ReportFromKep.FixedWidth = true;
GMAT ReportFromKep.Delimiter = ' ';
GMAT ReportFromKep.ColumnWidth = 23;
GMAT ReportFromKep.WriteReport = true;
%----------------------------------------
%---------- Mission Sequence
%----------------------------------------
BeginMissionSequence;
Propagate Synchronized DefaultProp(FromCart) DefaultProp(FromKep) {FromCart.ElapsedSecs = 0.0};