NavSatOrbit Class Reference
[GeoDynamics]

#include <NavSatOrbit.hpp>

Inheritance diagram for NavSatOrbit:

[legend]Collaboration diagram for NavSatOrbit:

[legend]List of all members.

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Detailed Description

This class handle equation of motion for navigation satellites.

Definition at line 46 of file NavSatOrbit.hpp.

Public Member Functions
	NavSatOrbit ()
	Default constructor.
virtual	~NavSatOrbit ()
	Default destructor.
virtual Vector< double >	getDerivatives (const double &t, const Vector< double > &y)
	Compute the derivatives.

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Constructor & Destructor Documentation

NavSatOrbit (   )

Default constructor. Definition at line 39 of file NavSatOrbit.cpp.

virtual ~NavSatOrbit (   )  [inline, virtual]

Default destructor. Definition at line 54 of file NavSatOrbit.hpp.

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Member Function Documentation

virtual Vector<double> getDerivatives (  const double &  t, const Vector< double > &  y )  [virtual]

Compute the derivatives. t time or the independent variable. y the required data. Returns: the derivatives. Reimplemented from SatOrbit.

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The documentation for this class was generated from the following files:

• NavSatOrbit.hpp
• NavSatOrbit.cpp

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