Merge branch 'master' of github.com:PX4/Firmware into asfilter

This commit is contained in:
Lorenz Meier 2014-07-29 11:09:44 +02:00
commit 628b735bc1
9 changed files with 55 additions and 31 deletions

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@ -736,6 +736,7 @@ int commander_thread_main(int argc, char *argv[])
// CIRCUIT BREAKERS
status.circuit_breaker_engaged_power_check = false;
status.circuit_breaker_engaged_airspd_check = false;
/* publish initial state */
status_pub = orb_advertise(ORB_ID(vehicle_status), &status);
@ -977,6 +978,7 @@ int commander_thread_main(int argc, char *argv[])
param_get(_param_component_id, &(status.component_id));
status.circuit_breaker_engaged_power_check = circuit_breaker_enabled("CBRK_SUPPLY_CHK", CBRK_SUPPLY_CHK_KEY);
status.circuit_breaker_engaged_airspd_check = circuit_breaker_enabled("CBRK_AIRSPD_CHK", CBRK_AIRSPD_CHK_KEY);
status_changed = true;

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@ -669,7 +669,9 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd)
goto system_eval;
}
if (!status->is_rotary_wing) {
/* Perform airspeed check only if circuit breaker is not
* engaged and it's not a rotary wing */
if (!status->circuit_breaker_engaged_airspd_check && !status->is_rotary_wing) {
/* accel done, close it */
close(fd);
fd = orb_subscribe(ORB_ID(airspeed));

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@ -630,10 +630,10 @@ FixedwingEstimator::check_filter_state()
rep.health_flags |= (((uint8_t)ekf_report.posHealth) << 1);
rep.health_flags |= (((uint8_t)ekf_report.hgtHealth) << 2);
rep.health_flags |= (((uint8_t)!ekf_report.gyroOffsetsExcessive) << 3);
// rep.health_flags |= (((uint8_t)ekf_report.onGround) << 4);
// rep.health_flags |= (((uint8_t)ekf_report.staticMode) << 5);
// rep.health_flags |= (((uint8_t)ekf_report.useCompass) << 6);
// rep.health_flags |= (((uint8_t)ekf_report.useAirspeed) << 7);
rep.health_flags |= (((uint8_t)ekf_report.onGround) << 4);
rep.health_flags |= (((uint8_t)ekf_report.staticMode) << 5);
rep.health_flags |= (((uint8_t)ekf_report.useCompass) << 6);
rep.health_flags |= (((uint8_t)ekf_report.useAirspeed) << 7);
rep.timeout_flags |= (((uint8_t)ekf_report.velTimeout) << 0);
rep.timeout_flags |= (((uint8_t)ekf_report.posTimeout) << 1);
@ -1465,25 +1465,6 @@ FixedwingEstimator::task_main()
_global_pos_pub = orb_advertise(ORB_ID(vehicle_global_position), &_global_pos);
}
if (hrt_elapsed_time(&_wind.timestamp) > 99000) {
_wind.timestamp = _global_pos.timestamp;
_wind.windspeed_north = _ekf->states[14];
_wind.windspeed_east = _ekf->states[15];
_wind.covariance_north = 0.0f; // XXX get form filter
_wind.covariance_east = 0.0f;
/* lazily publish the wind estimate only once available */
if (_wind_pub > 0) {
/* publish the wind estimate */
orb_publish(ORB_ID(wind_estimate), _wind_pub, &_wind);
} else {
/* advertise and publish */
_wind_pub = orb_advertise(ORB_ID(wind_estimate), &_wind);
}
}
if (hrt_elapsed_time(&_wind.timestamp) > 99000) {
_wind.timestamp = _global_pos.timestamp;
_wind.windspeed_north = _ekf->states[14];

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@ -3028,6 +3028,10 @@ void AttPosEKF::GetFilterState(struct ekf_status_report *err)
current_ekf_state.states[i] = states[i];
}
current_ekf_state.n_states = n_states;
current_ekf_state.onGround = onGround;
current_ekf_state.staticMode = staticMode;
current_ekf_state.useCompass = useCompass;
current_ekf_state.useAirspeed = useAirspeed;
memcpy(err, &current_ekf_state, sizeof(*err));

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@ -68,6 +68,10 @@ struct ekf_status_report {
bool posTimeout;
bool hgtTimeout;
bool imuTimeout;
bool onGround;
bool staticMode;
bool useCompass;
bool useAirspeed;
uint32_t velFailTime;
uint32_t posFailTime;
uint32_t hgtFailTime;

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@ -559,24 +559,41 @@ void Mavlink::mavlink_update_system(void)
_param_component_id = param_find("MAV_COMP_ID");
_param_system_type = param_find("MAV_TYPE");
_param_use_hil_gps = param_find("MAV_USEHILGPS");
_param_initialized = true;
}
/* update system and component id */
int32_t system_id;
param_get(_param_system_id, &system_id);
int32_t component_id;
param_get(_param_component_id, &component_id);
/* only allow system ID and component ID updates
* after reboot - not during operation */
if (!_param_initialized) {
if (system_id > 0 && system_id < 255) {
mavlink_system.sysid = system_id;
}
int32_t component_id;
param_get(_param_component_id, &component_id);
if (component_id > 0 && component_id < 255) {
mavlink_system.compid = component_id;
}
_param_initialized = true;
}
/* warn users that they need to reboot to take this
* into effect
*/
if (system_id != mavlink_system.sysid) {
send_statustext_critical("Save params and reboot to change SYSID");
}
if (component_id != mavlink_system.compid) {
send_statustext_critical("Save params and reboot to change COMPID");
}
int32_t system_type;
param_get(_param_system_type, &system_type);

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@ -83,6 +83,18 @@ PARAM_DEFINE_INT32(CBRK_RATE_CTRL, 0);
*/
PARAM_DEFINE_INT32(CBRK_IO_SAFETY, 0);
/**
* Circuit breaker for airspeed sensor
*
* Setting this parameter to 162128 will disable the check for an airspeed sensor.
* WARNING: ENABLING THIS CIRCUIT BREAKER IS AT OWN RISK
*
* @min 0
* @max 162128
* @group Circuit Breaker
*/
PARAM_DEFINE_INT32(CBRK_AIRSPD_CHK, 0);
bool circuit_breaker_enabled(const char* breaker, int32_t magic)
{
int32_t val;

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@ -52,6 +52,7 @@
#define CBRK_SUPPLY_CHK_KEY 894281
#define CBRK_RATE_CTRL_KEY 140253
#define CBRK_IO_SAFETY_KEY 22027
#define CBRK_AIRSPD_CHK_KEY 162128
#include <stdbool.h>

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@ -226,6 +226,7 @@ struct vehicle_status_s {
uint16_t errors_count4;
bool circuit_breaker_engaged_power_check;
bool circuit_breaker_engaged_airspd_check;
};
/**