lvlh_to_eci Class Reference

Convert LVLH initial conditions to ECI coordinates. More...

#include <lvlh_to_eci.h>

Inherits dsim_model.

Public Member Functions
	lvlh_to_eci (dsim_model_setup *setup)
	Constructor.
	~lvlh_to_eci ()
	Destructor.
void	initialize_data ()
	Initialize outlets and output variables.
void	initialization_complete ()
	Finish initialization.

Protected Attributes
dsim_variable	position_dsim
	Parent position.
dsim_variable	velocity_dsim
	Parent velocity.
dsim_variable	quaternion_dsim
	Parent quaternion.
dsim_variable	bodyRate_dsim
	Parent body rate matrix.

Detailed Description

Convert LVLH initial conditions to ECI coordinates.

Adding this model to your rigid body spacecraft allows you to specify the initial quaternion as the LVLH to body quaternion rather than the ECI to body quaternion. On initialization, this computes the LVLH to ECI quaternion from the spacecraft position and velocity and overwrites both the initial quaternion and the body rate to the corresponding ECI values.

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

• lvlh_to_eci.h
• lvlh_to_eci.cc