sc_data_names.h File Reference

Define the data names used throughout the control system. More...

#include <ControlDeck2/ControlDeck2.h>

Go to the source code of this file.

Classes
struct	sc_data
	Data point names and type. More...

Macros
#define	TYPED_DATA(x)   x.path, x.type
	Specify a data point with its type. More...
#define	q_eci_to_body_sim   "q_eci_to_body_sim"
	Simulation mapped variables. More...
#define	position_sim   "position_sim"
#define	velocity_sim   "velocity_sim"
#define	body_rate_camera_sim   "body_rate_camera_sim"
#define	inertia_sim   "inertia_sim"
#define	mass_sim   "mass_sim"
#define	center_of_mass_sim   "center_of_mass_sim"
#define	rwa_rate_sim   "rwa_rate_sim"
#define	centroid_camera_sim   "centroid_camera_sim"
#define	frame_camera_sim   "frame_camera_sim"
#define	gps_message_sim   "gps_message_sim"

Typedefs
typedef struct sc_data	SC_DATA
	Data point names and type. More...

Variables
Data Point Names
The data names are needed both when modules define data points and when other modules wish to access them. Therefore to provide compile-time detection of errors we define these names a priori.
const SC_DATA	acs_control_period_command = {"acs_control_period_command",sd_type_double}
	Most timers run after the ACS control period. More...
const SC_DATA	camera_data_command = {"camera_data_command",sd_type_matrix}
	Camera data command. More...
const SC_DATA	ephem_planet_mu = {"ephem_planet_mu",sd_type_matrix}
	Planet gravitational parameters. More...
const SC_DATA	ephem_observer = {"ephem_observer",sd_type_int}
	Ephemeris observer (int) More...
const SC_DATA	ephem_planet_rotation_matrix = {"ephem_planet_rotation_matrix",sd_type_matrix}
	Planet rotation matices. More...
const SC_DATA	ephem_planet_position = {"ephem_planet_position",sd_type_matrix}
	Planet position vectors. More...
const SC_DATA	ephem_planet_velocity = {"ephem_planet_velocity",sd_type_matrix}
	Planet velocities. More...
const SC_DATA	ephem_planet_index = {"ephem_planet_index",sd_type_matrix}
	Planet index. More...
const SC_DATA	ephem_planet_radius = {"ephem_planet_radius",sd_type_matrix}
	Planet radii. More...
const SC_DATA	ephem_sun_vector = {"ephem_sun_vector",sd_type_matrix}
	Sun unit vector. More...
const SC_DATA	star_visual_magnitude = {"star_visual_magnitude",sd_type_matrix}
	Star visual magnitudes, 1xn. More...
const SC_DATA	star_unit_vectors = {"star_unit_vectors",sd_type_matrix}
	Star unit vectors, 3xn. More...
const SC_DATA	ephem_hipparcos_ids = {"ephem_hipparcos_ids",sd_type_intarray}
	Star Hipparcos IDs, 1xn. More...
const SC_DATA	inertia = {"inertia",sd_type_matrix}
	Spacecraft inertia. More...
const SC_DATA	center_of_mass = {"center_of_mass",sd_type_matrix}
	Spacecraft center of mass. More...
const SC_DATA	mass = {"mass",sd_type_double}
	Spacecraft total mass (double) More...
const SC_DATA	julian_date = {"jd",sd_type_double}
	Julian date. More...
const SC_DATA	star_id_camera_1 = {"star_id_camera_1", sd_type_matrix}
const SC_DATA	u_star_camera_1 = {"u_star_camera_1", sd_type_matrix}
	Star unit vectors are a 3 by n matrix. More...
const SC_DATA	ad_q_eci_to_body = {"ad_q_eci_to_body", sd_type_matrix}
	Estimated inertial to body quaternion (4x1) More...
const SC_DATA	ad_initial_state_command = {"ad_initial_state_command", sd_type_matrix}
const SC_DATA	ad_gyro_bias_camera = {"ad_gyro_bias_camera", sd_type_matrix}
const SC_DATA	ad_covariance_camera = {"ad_covariance_camera", sd_type_matrix}
const SC_DATA	ad_q_eci_to_camera_single_frame = {"ad_q_eci_to_camera_single_frame", sd_type_matrix}
const SC_DATA	ad_parameter_command = {"ad_parameter_command", sd_type_matrix}
const SC_DATA	ad_plant_noise_covariance_command = {"ad_plant_noise_covariance_command", sd_type_matrix}
const SC_DATA	ad_meas_noise_covariance_command = {"ad_meas_noise_covariance_command", sd_type_matrix}
const SC_DATA	ad_initial_covariance_command = {"ad_initial_covariance_command", sd_type_matrix}
const SC_DATA	ad_reset_command = {"ad_reset_command", sd_type_int}
const SC_DATA	ad_use_single_frame_command = {"ad_use_single_frame_command", sd_type_int}
const SC_DATA	ad_q_camera_to_body_command = {"ad_q_camera_to_body_command", sd_type_matrix}
const SC_DATA	od_state = {"od:state", sd_type_matrix}
	Estimated orbit state (6x1 matrix). More...
const SC_DATA	camera_rate_meas = {"camera_rate_meas", sd_type_matrix}
const SC_DATA	star_data_1 = {"star_data_1", sd_type_matrix}
	Star data is a (4,n) matrix of [x;y;intensity;ID]. More...

Detailed Description

Define the data names used throughout the control system.

Macro Definition Documentation

q_eci_to_body_sim

#define q_eci_to_body_sim   "q_eci_to_body_sim"

Simulation mapped variables.

TYPED_DATA

#define TYPED_DATA

(

x

)

x.path, x.type

Specify a data point with its type.

Typedef Documentation

SC_DATA

typedef struct sc_data SC_DATA

Data point names and type.

Simple aggregate class.

Variable Documentation

acs_control_period_command

const SC_DATA acs_control_period_command = {"acs_control_period_command",sd_type_double}

Most timers run after the ACS control period.

Referenced by fsw_attitude_control::initialize_data(), and cs_timer::initialize_data_requests().

ad_q_eci_to_body

const SC_DATA ad_q_eci_to_body = {"ad_q_eci_to_body", sd_type_matrix}

Estimated inertial to body quaternion (4x1)

Referenced by fsw_attitude_determination::initialize_data(), and fsw_attitude_determination_ideal::initialize_data().

camera_data_command

const SC_DATA camera_data_command = {"camera_data_command",sd_type_matrix}

Camera data command.

center_of_mass

const SC_DATA center_of_mass = {"center_of_mass",sd_type_matrix}

Spacecraft center of mass.

Referenced by fsw_mass::initialize_data().

ephem_hipparcos_ids

const SC_DATA ephem_hipparcos_ids = {"ephem_hipparcos_ids",sd_type_intarray}

Star Hipparcos IDs, 1xn.

Referenced by fsw_star_catalog::initialize_data(), and fsw_star_catalog::initialize_star_catalog().

ephem_observer

const SC_DATA ephem_observer = {"ephem_observer",sd_type_int}

Ephemeris observer (int)

Referenced by fsw_ephemeris::initialize_data().

ephem_planet_index

const SC_DATA ephem_planet_index = {"ephem_planet_index",sd_type_matrix}

Planet index.

Referenced by fsw_ephemeris::initialize_data().

ephem_planet_mu

const SC_DATA ephem_planet_mu = {"ephem_planet_mu",sd_type_matrix}

Planet gravitational parameters.

Referenced by fsw_ephemeris::initialize_data().

ephem_planet_position

const SC_DATA ephem_planet_position = {"ephem_planet_position",sd_type_matrix}

Planet position vectors.

Referenced by fsw_ephemeris::initialize_data().

ephem_planet_radius

const SC_DATA ephem_planet_radius = {"ephem_planet_radius",sd_type_matrix}

Planet radii.

Referenced by fsw_ephemeris::initialize_data().

ephem_planet_rotation_matrix

const SC_DATA ephem_planet_rotation_matrix = {"ephem_planet_rotation_matrix",sd_type_matrix}

Planet rotation matices.

Referenced by fsw_ephemeris::initialize_data().

ephem_planet_velocity

const SC_DATA ephem_planet_velocity = {"ephem_planet_velocity",sd_type_matrix}

Planet velocities.

Referenced by fsw_ephemeris::initialize_data().

ephem_sun_vector

const SC_DATA ephem_sun_vector = {"ephem_sun_vector",sd_type_matrix}

Sun unit vector.

Referenced by fsw_ephemeris::initialize_data().

inertia

const SC_DATA inertia = {"inertia",sd_type_matrix}

Spacecraft inertia.

Referenced by fsw_euler_torque::handle_event(), and fsw_mass::initialize_data().

julian_date

const SC_DATA julian_date = {"jd",sd_type_double}

Julian date.

Referenced by cs_torquer_interface::handle_event(), fsw_star_catalog::handle_event(), fsw_star_catalog::initialize_data_requests(), and fsw_star_catalog::update_unit_vectors().

mass

const SC_DATA mass = {"mass",sd_type_double}

Spacecraft total mass (double)

Referenced by fsw_mass::initialize_data().

od_state

const SC_DATA od_state = {"od:state", sd_type_matrix}

Estimated orbit state (6x1 matrix).

Consists of [r;v] in km and km/s.

Parameters

path	"od_state"
type	sd_type_matrix

Referenced by fsw_attitude_determination_multi_sensor::handle_event(), fsw_attitude_determination_sun_star::handle_event(), fsw_ephemeris::handle_event(), and fsw_orbit_determination_ideal::initialize_data().

star_data_1

const SC_DATA star_data_1 = {"star_data_1", sd_type_matrix}

Star data is a (4,n) matrix of [x;y;intensity;ID].

star_unit_vectors

const SC_DATA star_unit_vectors = {"star_unit_vectors",sd_type_matrix}

Star unit vectors, 3xn.

Referenced by fsw_star_catalog::handle_event(), fsw_attitude_determination_least_squares::initialize(), fsw_star_catalog::initialize_data(), and fsw_star_catalog::initialize_star_catalog().

star_visual_magnitude

const SC_DATA star_visual_magnitude = {"star_visual_magnitude",sd_type_matrix}

Star visual magnitudes, 1xn.

Referenced by fsw_star_catalog::handle_event(), fsw_star_catalog::initialize_data(), and fsw_star_catalog::initialize_star_catalog().

u_star_camera_1

const SC_DATA u_star_camera_1 = {"u_star_camera_1", sd_type_matrix}

Star unit vectors are a 3 by n matrix.