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Public Member Functions |
| | Orbit () |
| virtual | ~Orbit () |
| void | SetStateObject (const OrbitState &_currentOrbitPosition) |
| | Set the current orbit state object that represents the spacecraft's position in space.
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| OrbitState | GetStateObject () const |
| | Return the current orbital state of the spacecraft.
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| void | SetDynamicsEq (odeFunctor _orbitDynamicsEq) |
| | Set the Dynamics Equation right-hand side file.
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| odeFunctor | GetDynamicsEq () |
| | Return the pointer to the Dynamics Equation right-hand side.
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| void | SetStateConversion (IntegratedOrbitStateConversionFunction _ConversionFunction) |
| | Set the Orbit state conversion function.
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| IntegratedOrbitStateConversionFunction | GetStateConversion () const |
| | Get the Orbit state conversion function.
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| void | SetPropagator (Propagator *_pPropagator) |
| | Sets the propagator used for integrating the orbit.
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| Propagator * | GetPropagator () |
| | Returns the pointer to the propagator being used.
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| void | Propagate (const Vector &_propTime) |
| | Propagate the orbit through the vector of times.
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| bool | IsIntegrateable () |
| | Returns whether the orbit is integrateable or not. Determined if there is a dynamics equation present.
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| void | SetParameters (const Matrix &_Parameters) |
| | Set the physical parameters of the spacecraft orbit.
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| Matrix | GetParameters () const |
| | Return a matrix of the current stored spacecraft orbital parameters.
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| void | SetEnvironment (Environment *_pEnvironment) |
| | Sets the environment used for integrating the orbit.
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| Environment * | GetEnvironment () |
| | Returns the environment used for integrating the orbit.
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| void | SetControlForces (const Vector &_controlForces) |
| Vector | GetControlForces () |
| ObjectFunctor< Environment > | GetEnvironmentForcesFunctor () |
| | Return a reference to the environmental forces function.
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| OrbitHistory & | GetHistoryObject () |
| | Return a reference to the spacecraft's orbit history.
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Protected Attributes |
| OrbitState | m_CurrentOrbitPosition |
| | Current stored orbital state of the spacecraft.
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Private Attributes |
| Propagator * | m_pPropagator |
| | Internal pointer to the current orbit propagator algorithm.
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| IntegratedOrbitStateConversionFunction | m_OrbitStateConversionFunction |
| odeFunctor | m_OrbitDynamicsEq |
| | Right-hand side of the orbit dynamics equation:  .
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| bool | m_Integrateable |
| | Is the orbit integrateable? (true if it is, false if is not).
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| Matrix | m_Parameters |
| Environment * | m_pEnvironment |
| | Internal pointer to the orbit's environment object.
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| Vector | m_ControlForces |
| | Internal Vector of the current control forces being applied to the spacecraft.
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| ObjectFunctor< Environment > | m_EnvironmentForcesFunctor |
| OrbitHistory | m_OrbitHistory |
1.3