Continuous state space system. More...

#include <state_space_vehicle.h>

Inherits dsim_model, and dsim_model.

Public Member Functions
void	initialize_data ()
	Initialize outlets and output variables.

void	initialization_complete ()
	Finish initialization.

void	initialize_timestep ()
	Computation done prior to numerical integration.

void	complete_timestep ()
	Computation done after numerical integration.

void	rhs (double t, double jd)
	Computation done during numerical integration. More...

void	initialize_data ()
	Initialize outlets and output variables.

void	initialization_complete ()
	Finish initialization.

void	initialize_timestep ()
	Computation done prior to numerical integration.

void	complete_timestep ()
	Computation done after numerical integration.

void	rhs (double t, double jd)
	Computation done during numerical integration.

Protected Attributes
Inputs
dsim_variable	u_dsim
	u vector

dsim_variable	y_dsim
	y vector

Parameters
dsim_variable	spacecraft_name_dsim
	Spacecraft name.

dsim_variable	spacecraft_type_dsim
	Spacecraft type.

dsim_variable	euler_index_dsim
	Index to Euler angles.

dsim_variable	omega_index_dsim
	Index to body rates.

dsim_variable	velocity_index_dsim
	Index to velocity.

dsim_variable	file_dsim
	File name.

Integrated states
dsim_variable	x_dsim
	State vector.

dsim_variable	position_dsim
	object position

dsim_variable	quaternion_dsim
	attitude quaternion ([scalar;x;y;z])

Outputs
dsim_variable	velocity_dsim
	object velocity

dsim_variable	bodyRate_dsim
	body rotational rates (rad/s)

state_space	s

Detailed Description

Continuous state space system.

State space vehicle model

$y = cx + du \dot{x} = ax + bu$

Uses the state_space class from the SCControl framework.

Member Function Documentation

Computation done during numerical integration.

State space model Right-Hand-Side.

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