cmd_InertialNavigationMagnetometerMeasurementUpdate.h

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/*
Inertial Navigation Magnetometer Measurement Update command definition header file
 
Author: James Tabony
*/
 
#ifndef COMMAND_CMD_INERTIAL_NAVIGATION_MAG_UPDATE_H
#define COMMAND_CMD_INERTIAL_NAVIGATION_MAG_UPDATE_H
 
#include "flight/Command.h"
#include "apps/app_apids.h"
 
// Define the command base for the inertial nav mag update app
#define CMD_GNC_INERT_NAV_MAG_UPDATE_BASE    APP_APID_GNC_INERT_NAV_MAG_UPDATE + CMD_APID_BASE
 
 
// -------------------------------------------------------------------------------------
// INERTIAL NAVIGATION MAGNETOMETER MEASUREMENT UPDATE COMMAND APID DEFINITIONS
// -------------------------------------------------------------------------------------
#define CMD_GNC_INERT_NAV_MAG_UPDATE_SET_NOISE    CMD_GNC_INERT_NAV_MAG_UPDATE_BASE + 0x000

COMMAND(cmd_gnc_inert_nav_mag_update_set_noise, CMD_GNC_INERT_NAV_MAG_UPDATE_SET_NOISE, 12,
    ((std::array<float, 3>), mag_std)   // New magnetic field vector measurement standard deviation resolved in magnetometer frame
) 
 
#endif