tlm_InertialNavigationBiasMeasurementUpdate.h

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/*
Inertial Navigation Bias Update telemetry definition header file
 
Author: James Tabony
*/
 
#ifndef TELEMETRY_TLM_INERTIAL_NAVIGATION_BIAS_UPDATE_H
#define TELEMETRY_TLM_INERTIAL_NAVIGATION_BIAS_UPDATE_H
 
#include "flight/Telemetry.h"
#include "apps/app_apids.h"
#include "apps/gnc/InertialNavigationEKF/InertialNavigationDefinition.hpp"
 
// Define the telemetry base for the Inertial Navigation EKF GPS Update Step
#define TLM_GNC_INERT_NAV_BIAS_UPDATE_BASE    APP_APID_GNC_INERT_NAV_BIAS_UPDATE + TLM_APID_BASE
 
// -------------------------------------------------------------------------------------
// INERTIAL NAVIGATION MAGNETOMETER MEASUREMENT UPDATE TELEMETRY APID DEFINITIONS
// -------------------------------------------------------------------------------------
#define TLM_GNC_A_POSTERIORI_STATE       TLM_GNC_INERT_NAV_BIAS_UPDATE_BASE + 0x000

TELEMETRY(tlm_gnc_a_posteriori_state, TLM_GNC_A_POSTERIORI_STATE, 64,
    ((std::array<float16, 16>), state_vector),
    ((std::array<float16, 16>), state_cov)
)
 
#endif