clockwerk::CalcXdotGravityJ2J3< T > Class Template Reference

Inheritance diagram for clockwerk::CalcXdotGravityJ2J3< T >:

Collaboration diagram for clockwerk::CalcXdotGravityJ2J3< T >:

Public Member Functions
int	calculateRates (T time, const std::array< T, 6 > &state, std::array< T, 6 > &out_rates)
	Function to calculate rate of change in 6-element orbit position with J2, J3.
virtual int	calculateRates (T time, const std::array< T, N > &state, std::array< T, N > &out_rates)
	Function to calculate rates from current state of system.

Public Attributes
T	mu
	The gravitational parameter for the planet. Must be set prior to calculation.
T	J2
	The J2 parameter for the planet. Must be set prior to calculation.
T	J3
	The J3 parameter for the planet. Must be set prior to calculation.
T	R
	The reference radius for the planet. Must be set prior to calculation.

Member Function Documentation

calculateRates() [1/2]

template<typename T >

int clockwerk::CalcXdotGravityJ2J3< T >::calculateRates	(	T	time,
		const std::array< T, 6 > &	state,
		std::array< T, 6 > &	out_rates
	)

Function to calculate rate of change in 6-element orbit position with J2, J3.

Parameters

time	The reference time
state	The state vector for the system as [x, y, z, xDot, yDot, zDot]
out_rates	Implicit return of rates based on time, state as [xDot, yDot, zDot, xDDot, yDDot, zDDot]

calculateRates() [2/2]

virtual int clockwerk::Rates< T, N >::calculateRates ( T  time, const std::array< T, N > &  state, std::array< T, N > &  out_rates  )

inlinevirtualinherited

Function to calculate rates from current state of system.

Parameters

time	The reference time
state	The reference state
out_rates	Implicit return of rates based on time, state

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

• /home/mickey/modelspace/clockwerk/src/gnc/navigation/dynamics/CalcXdotGravityJ2J3.hpp