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/*
This program is free software: you can redistribute it and/or modify
it under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
You should have received a copy of the GNU General Public License
along with this program. If not, see <http://www.gnu.org/licenses/>.
*/
/*
support for serial connected InertialLabs INS
*/
#include "AP_ExternalAHRS_config.h"
#if AP_EXTERNAL_AHRS_INERTIAL_LABS_ENABLED
#include "AP_ExternalAHRS_InertialLabs.h"
#include <AP_Math/AP_Math.h>
#include <AP_Math/crc.h>
#include <AP_Baro/AP_Baro.h>
#include <AP_Compass/AP_Compass.h>
#include <AP_GPS/AP_GPS.h>
#include <AP_Airspeed/AP_Airspeed.h>
#include <AP_InertialSensor/AP_InertialSensor.h>
#include <GCS_MAVLink/GCS.h>
#include <AP_Logger/AP_Logger.h>
#include <AP_SerialManager/AP_SerialManager.h>
#include <AP_HAL/utility/sparse-endian.h>
#include <AP_Common/Bitmask.h>
#include <AP_Vehicle/AP_Vehicle_Type.h>
extern const AP_HAL::HAL &hal;
// unit status bits
#define ILABS_UNIT_STATUS_ALIGNMENT_FAIL 0x0001
#define ILABS_UNIT_STATUS_OPERATION_FAIL 0x0002
#define ILABS_UNIT_STATUS_GYRO_FAIL 0x0004
#define ILABS_UNIT_STATUS_ACCEL_FAIL 0x0008
#define ILABS_UNIT_STATUS_MAG_FAIL 0x0010
#define ILABS_UNIT_STATUS_ELECTRONICS_FAIL 0x0020
#define ILABS_UNIT_STATUS_GNSS_FAIL 0x0040
#define ILABS_UNIT_STATUS_RUNTIME_CAL 0x0080
#define ILABS_UNIT_STATUS_VOLTAGE_LOW 0x0100
#define ILABS_UNIT_STATUS_VOLTAGE_HIGH 0x0200
#define ILABS_UNIT_STATUS_X_RATE_HIGH 0x0400
#define ILABS_UNIT_STATUS_Y_RATE_HIGH 0x0800
#define ILABS_UNIT_STATUS_Z_RATE_HIGH 0x1000
#define ILABS_UNIT_STATUS_MAG_FIELD_HIGH 0x2000
#define ILABS_UNIT_STATUS_TEMP_RANGE_ERR 0x4000
#define ILABS_UNIT_STATUS_RUNTIME_CAL2 0x8000
// unit status2 bits
#define ILABS_UNIT_STATUS2_ACCEL_X_HIGH 0x0001
#define ILABS_UNIT_STATUS2_ACCEL_Y_HIGH 0x0002
#define ILABS_UNIT_STATUS2_ACCEL_Z_HIGH 0x0004
#define ILABS_UNIT_STATUS2_BARO_FAIL 0x0008
#define ILABS_UNIT_STATUS2_DIFF_PRESS_FAIL 0x0010
#define ILABS_UNIT_STATUS2_MAGCAL_2D_ACT 0x0020
#define ILABS_UNIT_STATUS2_MAGCAL_3D_ACT 0x0020
#define ILABS_UNIT_STATUS2_GNSS_FUSION_OFF 0x0040
#define ILABS_UNIT_STATUS2_DIFF_PRESS_FUSION_OFF 0x0080
#define ILABS_UNIT_STATUS2_MAG_FUSION_OFF 0x0100
#define ILABS_UNIT_STATUS2_GNSS_POS_VALID 0x0200
// air data status bits
#define ILABS_AIRDATA_INIT_FAIL 0x0001
#define ILABS_AIRDATA_DIFF_PRESS_INIT_FAIL 0x0002
#define ILABS_AIRDATA_STATIC_PRESS_FAIL 0x0004
#define ILABS_AIRDATA_DIFF_PRESS_FAIL 0x0008
#define ILABS_AIRDATA_STATIC_PRESS_RANGE_ERR 0x0010
#define ILABS_AIRDATA_DIFF_PRESS_RANGE_ERR 0x0020
#define ILABS_AIRDATA_PRESS_ALT_FAIL 0x0040
#define ILABS_AIRDATA_AIRSPEED_FAIL 0x0080
#define ILABS_AIRDATA_BELOW_THRESHOLD 0x0100
// constructor
AP_ExternalAHRS_InertialLabs::AP_ExternalAHRS_InertialLabs(AP_ExternalAHRS *_frontend,
AP_ExternalAHRS::state_t &_state) :
AP_ExternalAHRS_backend(_frontend, _state)
{
auto &sm = AP::serialmanager();
uart = sm.find_serial(AP_SerialManager::SerialProtocol_AHRS, 0);
if (!uart) {
GCS_SEND_TEXT(MAV_SEVERITY_ERROR, "InertialLabs ExternalAHRS no UART");
return;
}
baudrate = sm.find_baudrate(AP_SerialManager::SerialProtocol_AHRS, 0);
port_num = sm.find_portnum(AP_SerialManager::SerialProtocol_AHRS, 0);
// don't offer IMU by default, at 200Hz it is too slow for many aircraft
set_default_sensors(uint16_t(AP_ExternalAHRS::AvailableSensor::GPS) |
uint16_t(AP_ExternalAHRS::AvailableSensor::BARO) |
uint16_t(AP_ExternalAHRS::AvailableSensor::COMPASS));
if (!hal.scheduler->thread_create(FUNCTOR_BIND_MEMBER(&AP_ExternalAHRS_InertialLabs::update_thread, void), "ILabs", 2048, AP_HAL::Scheduler::PRIORITY_SPI, 0)) {
AP_HAL::panic("InertialLabs Failed to start ExternalAHRS update thread");
}
GCS_SEND_TEXT(MAV_SEVERITY_INFO, "InertialLabs ExternalAHRS initialised");
}
/*
re-sync buffer on parse failure
*/
void AP_ExternalAHRS_InertialLabs::re_sync(void)
{
if (buffer_ofs > 3) {
/*
look for the 2 byte header and try to sync to that
*/
const uint16_t header = 0x55AA;
const uint8_t *p = (const uint8_t *)memmem(&buffer[1], buffer_ofs-3, &header, sizeof(header));
if (p != nullptr) {
const uint16_t n = p - &buffer[0];
memmove(&buffer[0], p, buffer_ofs - n);
buffer_ofs -= n;
} else {
buffer_ofs = 0;
}
} else {
buffer_ofs = 0;
}
}
// macro for checking we don't run past end of message buffer
#define CHECK_SIZE(d) need_re_sync = (message_ofs + (msg_len=sizeof(d)) > buffer_end); if (need_re_sync) break
// lookup a message in the msg_types bitmask to see if we received it in this packet
#define GOT_MSG(mtype) msg_types.get(unsigned(MessageType::mtype))
/*
check header is valid
*/
bool AP_ExternalAHRS_InertialLabs::check_header(const ILabsHeader *h) const
{
return h->magic == 0x55AA &&
h->msg_type == 1 &&
h->msg_id == 0x95 &&
h->msg_len <= sizeof(buffer)-2;
}
/*
check the UART for more data
returns true if we have consumed potentially valid bytes
*/
bool AP_ExternalAHRS_InertialLabs::check_uart()
{
WITH_SEMAPHORE(state.sem);
if (!setup_complete) {
return false;
}
uint32_t n = uart->available();
if (n == 0) {
return false;
}
if (n + buffer_ofs > sizeof(buffer)) {
n = sizeof(buffer) - buffer_ofs;
}
const ILabsHeader *h = (ILabsHeader *)&buffer[0];
if (buffer_ofs < sizeof(ILabsHeader)) {
n = MIN(n, sizeof(ILabsHeader)-buffer_ofs);
} else {
if (!check_header(h)) {
re_sync();
return false;
}
if (buffer_ofs > h->msg_len+8) {
re_sync();
return false;
}
n = MIN(n, uint32_t(h->msg_len + 2 - buffer_ofs));
}
const ssize_t nread = uart->read(&buffer[buffer_ofs], n);
if (nread != ssize_t(n)) {
re_sync();
return false;
}
buffer_ofs += n;
if (buffer_ofs < sizeof(ILabsHeader)) {
return true;
}
if (!check_header(h)) {
re_sync();
return false;
}
if (buffer_ofs < h->msg_len+2) {
/*
see if we can read the rest immediately
*/
const uint16_t needed = h->msg_len+2 - buffer_ofs;
if (uart->available() < needed) {
// need more data
return true;
}
const ssize_t nread2 = uart->read(&buffer[buffer_ofs], needed);
if (nread2 != needed) {
re_sync();
return false;
}
buffer_ofs += nread2;
}
// check checksum
const uint16_t crc1 = crc_sum_of_bytes_16(&buffer[2], buffer_ofs-4);
const uint16_t crc2 = le16toh_ptr(&buffer[buffer_ofs-2]);
if (crc1 != crc2) {
re_sync();
return false;
}
const uint8_t *buffer_end = &buffer[buffer_ofs];
const uint16_t payload_size = h->msg_len - 6;
const uint8_t *payload = &buffer[6];
if (payload_size < 3) {
re_sync();
return false;
}
const uint8_t num_messages = payload[0];
if (num_messages == 0 ||
num_messages > payload_size-1) {
re_sync();
return false;
}
const uint8_t *message_ofs = &payload[num_messages+1];
bool need_re_sync = false;
// bitmask for what types we get
Bitmask<256> msg_types;
uint32_t now_ms = AP_HAL::millis();
for (uint8_t i=0; i<num_messages; i++) {
if (message_ofs >= buffer_end) {
re_sync();
return false;
}
MessageType mtype = (MessageType)payload[1+i];
ILabsData &u = *(ILabsData*)message_ofs;
uint8_t msg_len = 0;
msg_types.set(unsigned(mtype));
switch (mtype) {
case MessageType::GPS_INS_TIME_MS: {
// this is the GPS tow timestamp in ms for when the IMU data was sampled
CHECK_SIZE(u.gps_time_ms);
state2.gnss_ins_time_ms = u.gps_time_ms;
break;
}
case MessageType::GPS_WEEK: {
CHECK_SIZE(u.gps_week);
gps_data.gps_week = u.gps_week;
break;
}
case MessageType::ACCEL_DATA_HR: {
CHECK_SIZE(u.accel_data_hr);
ins_data.accel = u.accel_data_hr.tofloat().rfu_to_frd()*GRAVITY_MSS*1.0e-6;
break;
}
case MessageType::GYRO_DATA_HR: {
CHECK_SIZE(u.gyro_data_hr);
ins_data.gyro = u.gyro_data_hr.tofloat().rfu_to_frd()*DEG_TO_RAD*1.0e-5;
break;
}
case MessageType::BARO_DATA: {
CHECK_SIZE(u.baro_data);
baro_data.pressure_pa = u.baro_data.pressure_pa2*2;
break;
}
case MessageType::MAG_DATA: {
CHECK_SIZE(u.mag_data);
mag_data.field = u.mag_data.tofloat().rfu_to_frd()*(10*NTESLA_TO_MGAUSS);
break;
}
case MessageType::ORIENTATION_ANGLES: {
CHECK_SIZE(u.orientation_angles);
state.quat.from_euler(radians(u.orientation_angles.roll*0.01),
radians(u.orientation_angles.pitch*0.01),
radians(u.orientation_angles.yaw*0.01));
state.have_quaternion = true;
if (last_att_ms == 0) {
GCS_SEND_TEXT(MAV_SEVERITY_INFO, "InertialLabs: got link");
}
last_att_ms = now_ms;
break;
}
case MessageType::VELOCITIES: {
CHECK_SIZE(u.velocity);
state.velocity = u.velocity.tofloat().rfu_to_frd()*0.01;
state.have_velocity = true;
last_vel_ms = now_ms;
break;
}
case MessageType::POSITION: {
CHECK_SIZE(u.position);
state.location.lat = u.position.lat;
state.location.lng = u.position.lon;
state.location.alt = u.position.alt;
state.have_location = true;
state.last_location_update_us = AP_HAL::micros();
last_pos_ms = now_ms;
break;
}
case MessageType::KF_VEL_COVARIANCE: {
CHECK_SIZE(u.kf_vel_covariance);
state2.kf_vel_covariance = u.kf_vel_covariance.tofloat() * 0.001;
break;
}
case MessageType::KF_POS_COVARIANCE: {
CHECK_SIZE(u.kf_pos_covariance);
state2.kf_pos_covariance = u.kf_pos_covariance.tofloat() * 0.001;
break;
}
case MessageType::UNIT_STATUS: {
CHECK_SIZE(u.unit_status);
state2.unit_status = u.unit_status;
break;
}
case MessageType::GNSS_EXTENDED_INFO: {
CHECK_SIZE(u.gnss_extended_info);
gps_data.fix_type = u.gnss_extended_info.fix_type+1;
state2.gnss_extended_info = u.gnss_extended_info;
break;
}
case MessageType::NUM_SATS: {
CHECK_SIZE(u.num_sats);
gps_data.satellites_in_view = u.num_sats;
break;
}
case MessageType::GNSS_POSITION: {
CHECK_SIZE(u.position);
gps_data.latitude = u.position.lat;
gps_data.longitude = u.position.lon;
gps_data.msl_altitude = u.position.alt;
break;
}
case MessageType::GNSS_VEL_TRACK: {
CHECK_SIZE(u.gnss_vel_track);
Vector2f velxy;
velxy.offset_bearing(u.gnss_vel_track.track_over_ground*0.01, u.gnss_vel_track.hor_speed*0.01);
gps_data.ned_vel_north = velxy.x;
gps_data.ned_vel_east = velxy.y;
gps_data.ned_vel_down = -u.gnss_vel_track.ver_speed*0.01;
break;
}
case MessageType::GNSS_POS_TIMESTAMP: {
CHECK_SIZE(u.gnss_pos_timestamp);
gps_data.ms_tow = u.gnss_pos_timestamp;
break;
}
case MessageType::GNSS_INFO_SHORT: {
CHECK_SIZE(u.gnss_info_short);
state2.gnss_info_short = u.gnss_info_short;
break;
}
case MessageType::GNSS_NEW_DATA: {
CHECK_SIZE(u.gnss_new_data);
state2.gnss_new_data = u.gnss_new_data;
break;
}
case MessageType::GNSS_JAM_STATUS: {
CHECK_SIZE(u.gnss_jam_status);
state2.gnss_jam_status = u.gnss_jam_status;
break;
}
case MessageType::DIFFERENTIAL_PRESSURE: {
CHECK_SIZE(u.differential_pressure);
airspeed_data.differential_pressure = u.differential_pressure*1.0e-4;
break;
}
case MessageType::TRUE_AIRSPEED: {
CHECK_SIZE(u.true_airspeed);
state2.true_airspeed = u.true_airspeed*0.01;
break;
}
case MessageType::WIND_SPEED: {
CHECK_SIZE(u.wind_speed);
state2.wind_speed = u.wind_speed.tofloat().rfu_to_frd()*0.01;
break;
}
case MessageType::AIR_DATA_STATUS: {
CHECK_SIZE(u.air_data_status);
state2.air_data_status = u.air_data_status;
break;
}
case MessageType::SUPPLY_VOLTAGE: {
CHECK_SIZE(u.supply_voltage);
state2.supply_voltage = u.supply_voltage*0.01;
break;
}
case MessageType::TEMPERATURE: {
CHECK_SIZE(u.temperature);
// assume same temperature for baro and airspeed
baro_data.temperature = u.temperature*0.1;
airspeed_data.temperature = u.temperature*0.1;
break;
}
case MessageType::UNIT_STATUS2: {
CHECK_SIZE(u.unit_status2);
state2.unit_status2 = u.unit_status2;
break;
}
}
if (msg_len == 0) {
// got an unknown message
GCS_SEND_TEXT(MAV_SEVERITY_INFO, "InertialLabs: unknown msg 0x%02x", unsigned(mtype));
buffer_ofs = 0;
return false;
}
message_ofs += msg_len;
if (msg_len == 0 || need_re_sync) {
re_sync();
return false;
}
}
if (h->msg_len != message_ofs-buffer) {
// we had stray bytes at the end of the message
re_sync();
return false;
}
if (GOT_MSG(ACCEL_DATA_HR) &&
GOT_MSG(GYRO_DATA_HR)) {
AP::ins().handle_external(ins_data);
}
if (GOT_MSG(GPS_INS_TIME_MS) &&
GOT_MSG(NUM_SATS) &&
GOT_MSG(GNSS_POSITION) &&
GOT_MSG(GNSS_NEW_DATA) &&
GOT_MSG(GNSS_EXTENDED_INFO) &&
state2.gnss_new_data != 0) {
uint8_t instance;
if (AP::gps().get_first_external_instance(instance)) {
AP::gps().handle_external(gps_data, instance);
}
if (gps_data.satellites_in_view > 3) {
if (last_gps_ms == 0) {
GCS_SEND_TEXT(MAV_SEVERITY_INFO, "InertialLabs: got GPS lock");
if (!state.have_origin) {
state.origin = Location{
gps_data.latitude,
gps_data.longitude,
gps_data.msl_altitude,
Location::AltFrame::ABSOLUTE};
state.have_origin = true;
}
}
last_gps_ms = now_ms;
}
}
if (GOT_MSG(BARO_DATA) &&
GOT_MSG(TEMPERATURE)) {
AP::baro().handle_external(baro_data);
}
if (GOT_MSG(MAG_DATA)) {
AP::compass().handle_external(mag_data);
}
#if AP_AIRSPEED_EXTERNAL_ENABLED && (APM_BUILD_COPTER_OR_HELI || APM_BUILD_TYPE(APM_BUILD_ArduPlane))
// only on plane and copter as others do not link AP_Airspeed
if (GOT_MSG(DIFFERENTIAL_PRESSURE) &&
GOT_MSG(TEMPERATURE)) {
auto *arsp = AP::airspeed();
if (arsp != nullptr) {
arsp->handle_external(airspeed_data);
}
}
#endif // AP_AIRSPEED_EXTERNAL_ENABLED
buffer_ofs = 0;
if (GOT_MSG(POSITION) &&
GOT_MSG(ORIENTATION_ANGLES) &&
GOT_MSG(VELOCITIES)) {
float roll, pitch, yaw;
state.quat.to_euler(roll, pitch, yaw);
uint64_t now_us = AP_HAL::micros64();
// @LoggerMessage: ILB1
// @Description: InertialLabs AHRS data1
// @Field: TimeUS: Time since system startup
// @Field: Roll: euler roll
// @Field: Pitch: euler pitch
// @Field: Yaw: euler yaw
// @Field: VN: velocity north
// @Field: VE: velocity east
// @Field: VD: velocity down
// @Field: Lat: latitude
// @Field: Lon: longitude
// @Field: Alt: altitude AMSL
AP::logger().WriteStreaming("ILB1", "TimeUS,Roll,Pitch,Yaw,VN,VE,VD,Lat,Lon,Alt",
"sdddnnnDUm",
"F000000GG0",
"QffffffLLf",
now_us,
degrees(roll), degrees(pitch), degrees(yaw),
state.velocity.x, state.velocity.y, state.velocity.z,
state.location.lat, state.location.lng, state.location.alt*0.01);
// @LoggerMessage: ILB2
// @Description: InertialLabs AHRS data2
// @Field: TimeUS: Time since system startup
// @Field: PosVarN: position variance north
// @Field: PosVarE: position variance east
// @Field: PosVarD: position variance down
// @Field: VelVarN: velocity variance north
// @Field: VelVarE: velocity variance east
// @Field: VelVarD: velocity variance down
AP::logger().WriteStreaming("ILB2", "TimeUS,PosVarN,PosVarE,PosVarD,VelVarN,VelVarE,VelVarD",
"smmmnnn",
"F000000",
"Qffffff",
now_us,
state2.kf_pos_covariance.x, state2.kf_pos_covariance.x, state2.kf_pos_covariance.z,
state2.kf_vel_covariance.x, state2.kf_vel_covariance.x, state2.kf_vel_covariance.z);
// @LoggerMessage: ILB3
// @Description: InertialLabs AHRS data3
// @Field: TimeUS: Time since system startup
// @Field: Stat1: unit status1
// @Field: Stat2: unit status2
// @Field: FType: fix type
// @Field: SpStat: spoofing status
// @Field: GI1: GNSS Info1
// @Field: GI2: GNSS Info2
// @Field: GJS: GNSS jamming status
// @Field: TAS: true airspeed
// @Field: WVN: Wind velocity north
// @Field: WVE: Wind velocity east
// @Field: WVD: Wind velocity down
AP::logger().WriteStreaming("ILB3", "TimeUS,Stat1,Stat2,FType,SpStat,GI1,GI2,GJS,TAS,WVN,WVE,WVD",
"s-----------",
"F-----------",
"QHHBBBBBffff",
now_us,
state2.unit_status, state2.unit_status2,
state2.gnss_extended_info.fix_type, state2.gnss_extended_info.spoofing_status,
state2.gnss_info_short.info1, state2.gnss_info_short.info2,
state2.gnss_jam_status,
state2.true_airspeed,
state2.wind_speed.x, state2.wind_speed.y, state2.wind_speed.z);
}
return true;
}
void AP_ExternalAHRS_InertialLabs::update_thread()
{
// Open port in the thread
uart->begin(baudrate, 1024, 512);
/*
we assume the user has already configured the device
*/
setup_complete = true;
while (true) {
if (!check_uart()) {
hal.scheduler->delay_microseconds(250);
}
}
}
// get serial port number for the uart
int8_t AP_ExternalAHRS_InertialLabs::get_port(void) const
{
if (!uart) {
return -1;
}
return port_num;
};
// accessors for AP_AHRS
bool AP_ExternalAHRS_InertialLabs::healthy(void) const
{
WITH_SEMAPHORE(state.sem);
return AP_HAL::millis() - last_att_ms < 100;
}
bool AP_ExternalAHRS_InertialLabs::initialised(void) const
{
if (!setup_complete) {
return false;
}
return true;
}
bool AP_ExternalAHRS_InertialLabs::pre_arm_check(char *failure_msg, uint8_t failure_msg_len) const
{
if (!setup_complete) {
hal.util->snprintf(failure_msg, failure_msg_len, "InertialLabs setup failed");
return false;
}
if (!healthy()) {
hal.util->snprintf(failure_msg, failure_msg_len, "InertialLabs unhealthy");
return false;
}
WITH_SEMAPHORE(state.sem);
uint32_t now = AP_HAL::millis();
if (now - last_att_ms > 10 ||
now - last_pos_ms > 10 ||
now - last_vel_ms > 10) {
hal.util->snprintf(failure_msg, failure_msg_len, "InertialLabs not up to date");
return false;
}
return true;
}
/*
get filter status. We don't know the meaning of the status bits yet,
so assume all OK if we have GPS lock
*/
void AP_ExternalAHRS_InertialLabs::get_filter_status(nav_filter_status &status) const
{
WITH_SEMAPHORE(state.sem);
uint32_t now = AP_HAL::millis();
const uint32_t dt_limit = 200;
const uint32_t dt_limit_gps = 500;
memset(&status, 0, sizeof(status));
const bool init_ok = (state2.unit_status & (ILABS_UNIT_STATUS_ALIGNMENT_FAIL|ILABS_UNIT_STATUS_OPERATION_FAIL))==0;
status.flags.initalized = init_ok;
status.flags.attitude = init_ok && (now - last_att_ms < dt_limit) && init_ok;
status.flags.vert_vel = init_ok && (now - last_vel_ms < dt_limit);
status.flags.vert_pos = init_ok && (now - last_pos_ms < dt_limit);
status.flags.horiz_vel = status.flags.vert_vel;
status.flags.horiz_pos_abs = status.flags.vert_pos;
status.flags.horiz_pos_rel = status.flags.horiz_pos_abs;
status.flags.pred_horiz_pos_rel = status.flags.horiz_pos_abs;
status.flags.pred_horiz_pos_abs = status.flags.horiz_pos_abs;
status.flags.using_gps = (now - last_gps_ms < dt_limit_gps) &&
(state2.unit_status & (ILABS_UNIT_STATUS_GNSS_FAIL|ILABS_UNIT_STATUS2_GNSS_FUSION_OFF)) == 0;
status.flags.gps_quality_good = (now - last_gps_ms < dt_limit_gps) &&
(state2.unit_status2 & ILABS_UNIT_STATUS2_GNSS_POS_VALID) != 0 &&
(state2.unit_status & ILABS_UNIT_STATUS_GNSS_FAIL) == 0;
status.flags.rejecting_airspeed = (state2.air_data_status & ILABS_AIRDATA_AIRSPEED_FAIL);
}
// send an EKF_STATUS message to GCS
void AP_ExternalAHRS_InertialLabs::send_status_report(GCS_MAVLINK &link) const
{
// prepare flags
uint16_t flags = 0;
nav_filter_status filterStatus;
get_filter_status(filterStatus);
if (filterStatus.flags.attitude) {
flags |= EKF_ATTITUDE;
}
if (filterStatus.flags.horiz_vel) {
flags |= EKF_VELOCITY_HORIZ;
}
if (filterStatus.flags.vert_vel) {
flags |= EKF_VELOCITY_VERT;
}
if (filterStatus.flags.horiz_pos_rel) {
flags |= EKF_POS_HORIZ_REL;
}
if (filterStatus.flags.horiz_pos_abs) {
flags |= EKF_POS_HORIZ_ABS;
}
if (filterStatus.flags.vert_pos) {
flags |= EKF_POS_VERT_ABS;
}
if (filterStatus.flags.terrain_alt) {
flags |= EKF_POS_VERT_AGL;
}
if (filterStatus.flags.const_pos_mode) {
flags |= EKF_CONST_POS_MODE;
}
if (filterStatus.flags.pred_horiz_pos_rel) {
flags |= EKF_PRED_POS_HORIZ_REL;
}
if (filterStatus.flags.pred_horiz_pos_abs) {
flags |= EKF_PRED_POS_HORIZ_ABS;
}
if (!filterStatus.flags.initalized) {
flags |= EKF_UNINITIALIZED;
}
// send message
const float vel_gate = 5;
const float pos_gate = 5;
const float hgt_gate = 5;
const float mag_var = 0;
mavlink_msg_ekf_status_report_send(link.get_chan(), flags,
state2.kf_vel_covariance.length()/vel_gate,
state2.kf_pos_covariance.xy().length()/pos_gate,
state2.kf_pos_covariance.z/hgt_gate,
mag_var, 0, 0);
}
#endif // AP_EXTERNAL_AHRS_INERTIAL_LABS_ENABLED
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