/*
do 10Hz logging
*/
void Plane::update_logging1(void)
{
if (should_log(MASK_LOG_ATTITUDE_MED) && !should_log(MASK_LOG_ATTITUDE_FAST)) {
Log_Write_Attitude();
}
if (should_log(MASK_LOG_ATTITUDE_MED) && !should_log(MASK_LOG_IMU))
Log_Write_IMU();
}
/*
log some key data - 10Hz
*/
void Rover::update_logging1(void)
{
if (should_log(MASK_LOG_ATTITUDE_MED) && !should_log(MASK_LOG_ATTITUDE_FAST))
Log_Write_Attitude();
if (should_log(MASK_LOG_CTUN))
Log_Write_Control_Tuning();
if (should_log(MASK_LOG_NTUN))
Log_Write_Nav_Tuning();
}
/*
do 10Hz logging
*/
void Plane::update_logging1(void)
{
if (should_log(MASK_LOG_ATTITUDE_MED) && !should_log(MASK_LOG_ATTITUDE_FAST)) {
Log_Write_Attitude();
}
if (should_log(MASK_LOG_ATTITUDE_MED) && !should_log(MASK_LOG_IMU))
DataFlash.Log_Write_IMU();
if (should_log(MASK_LOG_ATTITUDE_MED))
DataFlash.Log_Write_AOA_SSA(ahrs);
}
void Tracker::ten_hz_logging_loop()
{
if (should_log(MASK_LOG_IMU)) {
DataFlash.Log_Write_IMU();
}
if (should_log(MASK_LOG_ATTITUDE)) {
Log_Write_Attitude();
}
if (should_log(MASK_LOG_RCIN)) {
DataFlash.Log_Write_RCIN();
}
if (should_log(MASK_LOG_RCOUT)) {
DataFlash.Log_Write_RCOUT();
}
}
/*
log some key data - 10Hz
*/
void Rover::update_logging1(void)
{
if (should_log(MASK_LOG_ATTITUDE_MED) && !should_log(MASK_LOG_ATTITUDE_FAST)) {
Log_Write_Attitude();
}
if (should_log(MASK_LOG_THR)) {
Log_Write_Throttle();
DataFlash.Log_Write_Beacon(g2.beacon);
Log_Write_Proximity();
}
if (should_log(MASK_LOG_NTUN)) {
Log_Write_Nav_Tuning();
}
}
// twentyfive_hz_logging_loop
// should be run at 25hz
void Sub::twentyfive_hz_logging()
{
if (should_log(MASK_LOG_ATTITUDE_FAST)) {
Log_Write_Attitude();
DataFlash.Log_Write_Rate(ahrs, motors, attitude_control, pos_control);
if (should_log(MASK_LOG_PID)) {
DataFlash.Log_Write_PID(LOG_PIDR_MSG, attitude_control.get_rate_roll_pid().get_pid_info());
DataFlash.Log_Write_PID(LOG_PIDP_MSG, attitude_control.get_rate_pitch_pid().get_pid_info());
DataFlash.Log_Write_PID(LOG_PIDY_MSG, attitude_control.get_rate_yaw_pid().get_pid_info());
DataFlash.Log_Write_PID(LOG_PIDA_MSG, g.pid_accel_z.get_pid_info());
}
}
// log IMU data if we're not already logging at the higher rate
if (should_log(MASK_LOG_IMU) && !should_log(MASK_LOG_IMU_RAW)) {
DataFlash.Log_Write_IMU(ins);
}
}
// ten_hz_logging_loop
// should be run at 10hz
void Copter::ten_hz_logging_loop()
{
// log attitude data if we're not already logging at the higher rate
if (should_log(MASK_LOG_ATTITUDE_MED) && !should_log(MASK_LOG_ATTITUDE_FAST)) {
Log_Write_Attitude();
DataFlash.Log_Write_Rate(ahrs, motors, attitude_control, pos_control);
if (should_log(MASK_LOG_PID)) {
DataFlash.Log_Write_PID(LOG_PIDR_MSG, attitude_control.get_rate_roll_pid().get_pid_info());
DataFlash.Log_Write_PID(LOG_PIDP_MSG, attitude_control.get_rate_pitch_pid().get_pid_info());
DataFlash.Log_Write_PID(LOG_PIDY_MSG, attitude_control.get_rate_yaw_pid().get_pid_info());
DataFlash.Log_Write_PID(LOG_PIDA_MSG, g.pid_accel_z.get_pid_info() );
}
}
if (should_log(MASK_LOG_MOTBATT)) {
Log_Write_MotBatt();
}
if (should_log(MASK_LOG_RCIN)) {
DataFlash.Log_Write_RCIN();
if (rssi.enabled()) {
DataFlash.Log_Write_RSSI(rssi);
}
}
if (should_log(MASK_LOG_RCOUT)) {
DataFlash.Log_Write_RCOUT();
}
if (should_log(MASK_LOG_NTUN) && (mode_requires_GPS(control_mode) || landing_with_GPS())) {
Log_Write_Nav_Tuning();
}
if (should_log(MASK_LOG_IMU) || should_log(MASK_LOG_IMU_FAST) || should_log(MASK_LOG_IMU_RAW)) {
DataFlash.Log_Write_Vibration(ins);
}
if (should_log(MASK_LOG_CTUN)) {
attitude_control.control_monitor_log();
Log_Write_Proximity();
}
#if FRAME_CONFIG == HELI_FRAME
Log_Write_Heli();
#endif
}
// ten_hz_logging_loop
// should be run at 10hz
void Copter::ten_hz_logging_loop()
{
// log attitude data if we're not already logging at the higher rate
if (should_log(MASK_LOG_ATTITUDE_MED) && !should_log(MASK_LOG_ATTITUDE_FAST)) {
Log_Write_Attitude();
Log_Write_EKF_POS();
}
if (should_log(MASK_LOG_MOTBATT)) {
Log_Write_MotBatt();
}
if (should_log(MASK_LOG_RCIN)) {
DataFlash.Log_Write_RCIN();
if (rssi.enabled()) {
DataFlash.Log_Write_RSSI(rssi);
}
}
if (should_log(MASK_LOG_RCOUT)) {
DataFlash.Log_Write_RCOUT();
}
if (should_log(MASK_LOG_NTUN) && (flightmode->requires_GPS() || landing_with_GPS())) {
pos_control->write_log();
}
if (should_log(MASK_LOG_IMU) || should_log(MASK_LOG_IMU_FAST) || should_log(MASK_LOG_IMU_RAW)) {
DataFlash.Log_Write_Vibration();
}
if (should_log(MASK_LOG_CTUN)) {
attitude_control->control_monitor_log();
#if PROXIMITY_ENABLED == ENABLED
DataFlash.Log_Write_Proximity(g2.proximity); // Write proximity sensor distances
#endif
#if BEACON_ENABLED == ENABLED
DataFlash.Log_Write_Beacon(g2.beacon);
#endif
}
#if FRAME_CONFIG == HELI_FRAME
Log_Write_Heli();
#endif
}
// update AHRS system
void Plane::ahrs_update()
{
hal.util->set_soft_armed(arming.is_armed() &&
hal.util->safety_switch_state() != AP_HAL::Util::SAFETY_DISARMED);
#if HIL_SUPPORT
if (g.hil_mode == 1) {
// update hil before AHRS update
gcs_update();
}
#endif
ahrs.update();
if (should_log(MASK_LOG_ATTITUDE_FAST)) {
Log_Write_Attitude();
}
if (should_log(MASK_LOG_IMU)) {
Log_Write_IMU();
DataFlash.Log_Write_IMUDT(ins);
}
// calculate a scaled roll limit based on current pitch
roll_limit_cd = g.roll_limit_cd * cosf(ahrs.pitch);
pitch_limit_min_cd = aparm.pitch_limit_min_cd * fabsf(cosf(ahrs.roll));
// updated the summed gyro used for ground steering and
// auto-takeoff. Dot product of DCM.c with gyro vector gives earth
// frame yaw rate
steer_state.locked_course_err += ahrs.get_yaw_rate_earth() * G_Dt;
steer_state.locked_course_err = wrap_PI(steer_state.locked_course_err);
// update inertial_nav for quadplane
quadplane.inertial_nav.update(G_Dt);
}
// update AHRS system
void Rover::ahrs_update()
{
update_soft_armed();
#if HIL_MODE != HIL_MODE_DISABLED
// update hil before AHRS update
gcs_update();
#endif
// AHRS may use movement to calculate heading
update_ahrs_flyforward();
ahrs.update();
// update position
have_position = ahrs.get_position(current_loc);
// update home from EKF if necessary
update_home_from_EKF();
// if using the EKF get a speed update now (from accelerometers)
Vector3f velocity;
if (ahrs.get_velocity_NED(velocity)) {
ground_speed = norm(velocity.x, velocity.y);
} else if (gps.status() >= AP_GPS::GPS_OK_FIX_3D) {
ground_speed = ahrs.groundspeed();
}
if (should_log(MASK_LOG_ATTITUDE_FAST)) {
Log_Write_Attitude();
}
if (should_log(MASK_LOG_IMU)) {
DataFlash.Log_Write_IMU();
}
}
// Full rate logging of attitude, rate and pid loops
// should be run at 400hz
void Copter::fourhundred_hz_logging()
{
if (should_log(MASK_LOG_ATTITUDE_FAST)) {
Log_Write_Attitude();
}
}
// do logging at loop rate
void Plane::Log_Write_Fast(void)
{
if (should_log(MASK_LOG_ATTITUDE_FAST)) {
Log_Write_Attitude();
}
}
