HokieSatSimulation.h Source File

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00010 // Standard includes
00011 #include "Matrix.h"
00012 #include "Rotation.h"
00013 
00014 // Dynamics includes
00015 #include "CombinedNumericPropagator.h"
00016 #include "RungeKuttaFehlbergIntegrator.h"
00017 
00018 // Orbit Includes
00019 #include "Orbit.h"
00020 #include "OrbitState.h"
00021 #include "orbitmodels/TwoBodyDynamics.h"
00022 #include "orbitstaterep/PositionVelocity.h"
00023 #include "orbitframes/OrbitFrameIJK.h"
00024 
00025 // Attitude includes
00026 #include "Attitude.h"
00027 #include "AttitudeState.h"
00028 #include "AttitudeModels/QuaternionAngVelDynamics.h"
00029 
00030 // Environment Includes
00031 #include "CentralBody/EarthCentralBody.h"
00032 #include "CentralBody/Models/TiltedDipoleMagneticModel.h"
00033 #include "Disturbances/GravityFunctions.h"
00034 #include "Disturbances/SimpleAerodynamicDisturbances.h"
00035 
00036 // Utility Includes
00037 #include "Plot.h"
00038 #include "MathUtils.h"
00039 
00040 using namespace O_SESSAME;
00041 
00043 NumericPropagator* SetupPropagator();
00046 Environment* SetupEnvironment(Attitude* pSatAttitude);
00047 
00049 Orbit* SetupOrbit();
00050 
00052 Attitude* SetupAttitude();
00053 
00057 Vector ControlTorques(Matrix CurrentAttState, Matrix DesAttState, double epoch, double count);