Merge pull request #2175 from Zefz/preflight_gps_check

Preflight: GPS check
This commit is contained in:
Lorenz Meier
2015-05-19 10:10:46 +02:00
7 changed files with 119 additions and 39 deletions

View File

@@ -303,6 +303,18 @@ then
#
sh /etc/init.d/rc.sensors
if [ $GPS == yes ]
then
if [ $GPS_FAKE == yes ]
then
echo "[i] Faking GPS"
gps start -f
else
gps start
fi
fi
unset GPS_FAKE
# Needs to be this early for in-air-restarts
commander start
@@ -479,22 +491,10 @@ then
sh /etc/init.d/rc.uavcan
#
# Logging, GPS
# Logging
#
sh /etc/init.d/rc.logging
if [ $GPS == yes ]
then
if [ $GPS_FAKE == yes ]
then
echo "[i] Faking GPS"
gps start -f
else
gps start
fi
fi
unset GPS_FAKE
#
# Start up ARDrone Motor interface
#

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@@ -354,6 +354,20 @@ GPS::task_main()
if (_Helper->configure(_baudrate) == 0) {
unlock();
//Publish initial report that we have access to a GPS
//Make sure to clear any stale data in case driver is reset
memset(&_report_gps_pos, 0, sizeof(_report_gps_pos));
_report_gps_pos.timestamp_position = hrt_absolute_time();
_report_gps_pos.timestamp_variance = hrt_absolute_time();
_report_gps_pos.timestamp_velocity = hrt_absolute_time();
_report_gps_pos.timestamp_time = hrt_absolute_time();
if (_report_gps_pos_pub > 0) {
orb_publish(ORB_ID(vehicle_gps_position), _report_gps_pos_pub, &_report_gps_pos);
} else {
_report_gps_pos_pub = orb_advertise(ORB_ID(vehicle_gps_position), &_report_gps_pos);
}
// GPS is obviously detected successfully, reset statistics
_Helper->reset_update_rates();
@@ -364,13 +378,7 @@ GPS::task_main()
if (!(_pub_blocked)) {
if (helper_ret & 1) {
if (_report_gps_pos_pub > 0) {
orb_publish(ORB_ID(vehicle_gps_position), _report_gps_pos_pub, &_report_gps_pos);
} else {
_report_gps_pos_pub = orb_advertise(ORB_ID(vehicle_gps_position), &_report_gps_pos);
}
orb_publish(ORB_ID(vehicle_gps_position), _report_gps_pos_pub, &_report_gps_pos);
}
if (_p_report_sat_info && (helper_ret & 2)) {
if (_report_sat_info_pub > 0) {

View File

@@ -48,6 +48,7 @@
#include <fcntl.h>
#include <errno.h>
#include <math.h>
#include <poll.h>
#include <systemlib/err.h>
#include <systemlib/param/param.h>
@@ -61,6 +62,7 @@
#include <drivers/drv_airspeed.h>
#include <uORB/topics/airspeed.h>
#include <uORB/topics/vehicle_gps_position.h>
#include <mavlink/mavlink_log.h>
@@ -269,8 +271,38 @@ out:
return success;
}
static bool gnssCheck(int mavlink_fd)
{
bool success = true;
int gpsSub = orb_subscribe(ORB_ID(vehicle_gps_position));
//Wait up to 2000ms to allow the driver to detect a GNSS receiver module
struct pollfd fds[1];
fds[0].fd = gpsSub;
fds[0].events = POLLIN;
if(poll(fds, 1, 2000) <= 0) {
success = false;
}
else {
struct vehicle_gps_position_s gps;
if ( (OK != orb_copy(ORB_ID(vehicle_gps_position), gpsSub, &gps)) ||
(hrt_elapsed_time(&gps.timestamp_position) > 1000000)) {
success = false;
}
}
//Report failure to detect module
if(!success) {
mavlink_and_console_log_critical(mavlink_fd, "PREFLIGHT FAIL: GPS RECEIVER MISSING");
}
close(gpsSub);
return success;
}
bool preflightCheck(int mavlink_fd, bool checkMag, bool checkAcc, bool checkGyro,
bool checkBaro, bool checkAirspeed, bool checkRC, bool checkDynamic)
bool checkBaro, bool checkAirspeed, bool checkRC, bool checkGNSS, bool checkDynamic)
{
bool failed = false;
@@ -336,6 +368,13 @@ bool preflightCheck(int mavlink_fd, bool checkMag, bool checkAcc, bool checkGyro
}
}
/* ---- Global Navigation Satellite System receiver ---- */
if(checkGNSS) {
if(!gnssCheck(mavlink_fd)) {
failed = true;
}
}
/* Report status */
return !failed;
}

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@@ -59,11 +59,15 @@ namespace Commander
* true if the gyroscopes should be checked
* @param checkBaro
* true if the barometer should be checked
* @param checkAirspeed
* true if the airspeed sensor should be checked
* @param checkRC
* true if the Remote Controller should be checked
* @param checkGNSS
* true if the GNSS receiver should be checked
**/
bool preflightCheck(int mavlink_fd, bool checkMag, bool checkAcc,
bool checkGyro, bool checkBaro, bool checkAirspeed, bool checkRC, bool checkDynamic = false);
bool checkGyro, bool checkBaro, bool checkAirspeed, bool checkRC, bool checkGNSS, bool checkDynamic = false);
const unsigned max_mandatory_gyro_count = 1;
const unsigned max_optional_gyro_count = 3;

View File

@@ -125,6 +125,8 @@ static const int ERROR = -1;
extern struct system_load_s system_load;
static constexpr uint8_t COMMANDER_MAX_GPS_NOISE = 60; /**< Maximum percentage signal to noise ratio allowed for GPS reception */
/* Decouple update interval and hysteris counters, all depends on intervals */
#define COMMANDER_MONITORING_INTERVAL 50000
#define COMMANDER_MONITORING_LOOPSPERMSEC (1/(COMMANDER_MONITORING_INTERVAL/1000.0f))
@@ -916,6 +918,7 @@ int commander_thread_main(int argc, char *argv[])
status.circuit_breaker_engaged_airspd_check = false;
status.circuit_breaker_engaged_enginefailure_check = false;
status.circuit_breaker_engaged_gpsfailure_check = false;
get_circuit_breaker_params();
/* publish initial state */
status_pub = orb_advertise(ORB_ID(vehicle_status), &status);
@@ -1117,8 +1120,6 @@ int commander_thread_main(int argc, char *argv[])
param_get(_param_sys_type, &(status.system_type)); // get system type
status.is_rotary_wing = is_rotary_wing(&status) || is_vtol(&status);
get_circuit_breaker_params();
bool checkAirspeed = false;
/* Perform airspeed check only if circuit breaker is not
* engaged and it's not a rotary wing */
@@ -1127,7 +1128,7 @@ int commander_thread_main(int argc, char *argv[])
}
// Run preflight check
status.condition_system_sensors_initialized = Commander::preflightCheck(mavlink_fd, true, true, true, true, checkAirspeed, true);
status.condition_system_sensors_initialized = Commander::preflightCheck(mavlink_fd, true, true, true, true, checkAirspeed, true, !status.circuit_breaker_engaged_gpsfailure_check);
if (!status.condition_system_sensors_initialized) {
set_tune_override(TONE_GPS_WARNING_TUNE); //sensor fail tune
}
@@ -1300,7 +1301,7 @@ int commander_thread_main(int argc, char *argv[])
}
/* provide RC and sensor status feedback to the user */
(void)Commander::preflightCheck(mavlink_fd, true, true, true, true, chAirspeed, true);
(void)Commander::preflightCheck(mavlink_fd, true, true, true, true, chAirspeed, true, !status.circuit_breaker_engaged_gpsfailure_check);
}
telemetry_last_heartbeat[i] = telemetry.heartbeat_time;
@@ -1637,19 +1638,31 @@ int commander_thread_main(int argc, char *argv[])
(float)gps_position.alt * 1.0e-3f, hrt_absolute_time());
}
/* check if GPS fix is ok */
if (status.circuit_breaker_engaged_gpsfailure_check ||
(gps_position.fix_type >= 3 &&
hrt_elapsed_time(&gps_position.timestamp_position) < FAILSAFE_DEFAULT_TIMEOUT)) {
/* handle the case where gps was regained */
if (status.gps_failure) {
status.gps_failure = false;
status_changed = true;
mavlink_log_critical(mavlink_fd, "gps regained");
/* check if GPS is ok */
if (!status.circuit_breaker_engaged_gpsfailure_check) {
bool gpsIsNoisy = gps_position.noise_per_ms > 0 && gps_position.noise_per_ms < COMMANDER_MAX_GPS_NOISE;
//Check if GPS receiver is too noisy while we are disarmed
if (!armed.armed && gpsIsNoisy) {
if (!status.gps_failure) {
mavlink_log_critical(mavlink_fd, "GPS signal noisy");
set_tune_override(TONE_GPS_WARNING_TUNE);
//GPS suffers from signal jamming or excessive noise, disable GPS-aided flight
status.gps_failure = true;
status_changed = true;
}
}
} else {
if (!status.gps_failure) {
if (gps_position.fix_type >= 3 && hrt_elapsed_time(&gps_position.timestamp_position) < FAILSAFE_DEFAULT_TIMEOUT) {
/* handle the case where gps was regained */
if (status.gps_failure && !gpsIsNoisy) {
status.gps_failure = false;
status_changed = true;
mavlink_log_critical(mavlink_fd, "gps regained");
}
} else if (!status.gps_failure) {
status.gps_failure = true;
status_changed = true;
mavlink_log_critical(mavlink_fd, "gps fix lost");
@@ -2751,7 +2764,7 @@ void *commander_low_prio_loop(void *arg)
checkAirspeed = true;
}
status.condition_system_sensors_initialized = Commander::preflightCheck(mavlink_fd, true, true, true, true, checkAirspeed, true);
status.condition_system_sensors_initialized = Commander::preflightCheck(mavlink_fd, true, true, true, true, checkAirspeed, true, !status.circuit_breaker_engaged_gpsfailure_check);
arming_state_transition(&status, &safety, vehicle_status_s::ARMING_STATE_STANDBY, &armed, true /* fRunPreArmChecks */, mavlink_fd);

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@@ -689,5 +689,5 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd)
checkAirspeed = true;
}
return !Commander::preflightCheck(mavlink_fd, true, true, true, true, checkAirspeed, true, true);
return !Commander::preflightCheck(mavlink_fd, true, true, true, true, checkAirspeed, true, !status->circuit_breaker_engaged_gpsfailure_check, true);
}

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@@ -120,3 +120,19 @@ PARAM_DEFINE_INT32(CBRK_FLIGHTTERM, 121212);
* @group Circuit Breaker
*/
PARAM_DEFINE_INT32(CBRK_ENGINEFAIL, 284953);
/**
* Circuit breaker for GPS failure detection
*
* Setting this parameter to 240024 will disable the GPS failure detection.
* If this check is enabled, then the sensor check will fail if the GPS module
* is missing. It will also check for excessive signal noise on the GPS receiver
* and warn the user if detected.
*
* WARNING: ENABLING THIS CIRCUIT BREAKER IS AT OWN RISK
*
* @min 0
* @max 240024
* @group Circuit Breaker
*/
PARAM_DEFINE_INT32(CBRK_GPSFAIL, 240024);