forked from Archive/PX4-Autopilot
Subsystem_info status flags & checks : Initial commit, updating the health flags in a centralized way mostly in commander and the votedSensorsUpdate function.
This commit is contained in:
parent
40e6a5a39b
commit
6f1f414b49
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@ -11,10 +11,21 @@ uint64 SUBSYSTEM_TYPE_EXTERNALGROUNDTRUTH = 512
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uint64 SUBSYSTEM_TYPE_ANGULARRATECONTROL = 1024
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uint64 SUBSYSTEM_TYPE_ATTITUDESTABILIZATION = 2048
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uint64 SUBSYSTEM_TYPE_YAWPOSITION = 4096
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uint64 SUBSYSTEM_TYPE_ALTITUDECONTROL = 16384
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uint64 SUBSYSTEM_TYPE_POSITIONCONTROL = 32768
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uint64 SUBSYSTEM_TYPE_MOTORCONTROL = 65536
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uint64 SUBSYSTEM_TYPE_RANGEFINDER = 131072
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uint64 SUBSYSTEM_TYPE_ALTITUDECONTROL = 8192
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uint64 SUBSYSTEM_TYPE_POSITIONCONTROL = 16384
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uint64 SUBSYSTEM_TYPE_MOTORCONTROL = 32768
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uint64 SUBSYSTEM_TYPE_RCRECEIVER = 65536
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uint64 SUBSYSTEM_TYPE_GYRO2 = 131072
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uint64 SUBSYSTEM_TYPE_ACC2 = 262144
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uint64 SUBSYSTEM_TYPE_MAG2 = 524288
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uint64 SUBSYSTEM_TYPE_GEOFENCE = 1048576
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uint64 SUBSYSTEM_TYPE_AHRS = 2097152
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uint64 SUBSYSTEM_TYPE_TERRAIN = 4194304
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uint64 SUBSYSTEM_TYPE_REVERSEMOTOR = 8388608
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uint64 SUBSYSTEM_TYPE_LOGGING = 16777216
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uint64 SUBSYSTEM_TYPE_SENSORBATTERY = 33554432
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uint64 SUBSYSTEM_TYPE_SENSORPROXIMITY = 67108864
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uint64 SUBSYSTEM_TYPE_MISSION = 134217728
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bool present
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bool enabled
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@ -27,5 +27,6 @@ bool offboard_control_loss_timeout # true if offboard is lost for
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bool rc_signal_found_once
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bool rc_input_blocked # set if RC input should be ignored temporarily
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bool rc_calibration_valid # set if RC calibration is valid
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bool vtol_transition_failure # Set to true if vtol transition failed
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bool usb_connected # status of the USB power supply
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@ -53,7 +53,6 @@
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#include <px4_workqueue.h>
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#include <perf/perf_counter.h>
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#include <uORB/topics/battery_status.h>
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#include <uORB/topics/subsystem_info.h>
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#include <uORB/uORB.h>
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#define BATT_SMBUS_ADDR_MIN 0x00 ///< lowest possible address
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@ -54,7 +54,6 @@
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#include <uORB/uORB.h>
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#include <uORB/topics/differential_pressure.h>
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#include <uORB/topics/subsystem_info.h>
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#include <drivers/airspeed/airspeed.h>
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/* I2C bus address */
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@ -66,7 +66,6 @@
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#include <uORB/uORB.h>
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#include <uORB/topics/differential_pressure.h>
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#include <uORB/topics/subsystem_info.h>
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#include <uORB/topics/system_power.h>
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#include <drivers/airspeed/airspeed.h>
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@ -58,6 +58,7 @@
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#include <perf/perf_counter.h>
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#include <systemlib/err.h>
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#include <systemlib/subsystem_info_pub.h>
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#include <drivers/drv_hrt.h>
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#include <drivers/drv_range_finder.h>
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@ -73,7 +74,6 @@
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/* Configuration Constants */
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#define SR04_DEVICE_PATH "/dev/hc_sr04"
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#define SUBSYSTEM_TYPE_RANGEFINDER 131072
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/* Device limits */
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#define SR04_MIN_DISTANCE (0.10f)
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#define SR04_MAX_DISTANCE (4.00f)
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@ -626,22 +626,7 @@ HC_SR04::start()
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/* notify about state change */
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struct subsystem_info_s info = {};
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info.present = true;
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info.enabled = true;
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info.ok = true;
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info.subsystem_type = SUBSYSTEM_TYPE_RANGEFINDER;
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static orb_advert_t pub = nullptr;
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if (pub != nullptr) {
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orb_publish(ORB_ID(subsystem_info), pub, &info);
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} else {
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pub = orb_advertise(ORB_ID(subsystem_info), &info);
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}
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publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_SENSORPROXIMITY, true, true, true);
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}
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void
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@ -61,6 +61,7 @@
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#include <perf/perf_counter.h>
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#include <systemlib/err.h>
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#include <systemlib/subsystem_info_pub.h>
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#include <drivers/drv_hrt.h>
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#include <drivers/drv_range_finder.h>
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@ -590,22 +591,7 @@ MB12XX::start()
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work_queue(HPWORK, &_work, (worker_t)&MB12XX::cycle_trampoline, this, 5);
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/* notify about state change */
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struct subsystem_info_s info = {};
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info.present = true;
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info.enabled = true;
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info.ok = true;
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info.subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_RANGEFINDER;
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static orb_advert_t pub = nullptr;
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if (pub != nullptr) {
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orb_publish(ORB_ID(subsystem_info), pub, &info);
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} else {
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pub = orb_advertise(ORB_ID(subsystem_info), &info);
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}
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publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_SENSORPROXIMITY, true, true, true);
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}
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void
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@ -66,7 +66,6 @@
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#include <drivers/device/ringbuffer.h>
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#include <uORB/uORB.h>
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#include <uORB/topics/subsystem_info.h>
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#include <uORB/topics/distance_sensor.h>
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#include "sf0x_parser.h"
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@ -645,20 +644,7 @@ SF0X::start()
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work_queue(HPWORK, &_work, (worker_t)&SF0X::cycle_trampoline, this, 1);
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// /* notify about state change */
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// struct subsystem_info_s info = {
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// true,
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// true,
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// true,
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// SUBSYSTEM_TYPE_RANGEFINDER
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// };
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// static orb_advert_t pub = -1;
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// if (pub > 0) {
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// orb_publish(ORB_ID(subsystem_info), pub, &info);
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// } else {
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// pub = orb_advertise(ORB_ID(subsystem_info), &info);
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// }
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// publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_SENSORPROXIMITY, true, true, true);
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}
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void
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@ -64,12 +64,14 @@
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#include <perf/perf_counter.h>
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#include <systemlib/err.h>
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#include <systemlib/subsystem_info_pub.h>
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#include <drivers/drv_hrt.h>
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#include <drivers/drv_range_finder.h>
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#include <drivers/device/ringbuffer.h>
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#include <uORB/uORB.h>
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#include <uORB/topics/subsystem_info.h>
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#include <uORB/topics/distance_sensor.h>
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#include <board_config.h>
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@ -584,6 +586,9 @@ SF1XX::start()
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/* schedule a cycle to start things */
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work_queue(HPWORK, &_work, (worker_t)&SF1XX::cycle_trampoline, this, USEC2TICK(_conversion_interval));
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/* notify about state change */
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publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_SENSORPROXIMITY, true, true, true);
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}
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void
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@ -60,6 +60,7 @@
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#include <perf/perf_counter.h>
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#include <systemlib/err.h>
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#include <systemlib/subsystem_info_pub.h>
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#include <drivers/drv_hrt.h>
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#include <drivers/drv_range_finder.h>
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@ -593,22 +594,7 @@ SRF02::start()
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work_queue(HPWORK, &_work, (worker_t)&SRF02::cycle_trampoline, this, 5);
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/* notify about state change */
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struct subsystem_info_s info = {};
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info.present = true;
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info.enabled = true;
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info.ok = true;
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info.subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_RANGEFINDER;
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static orb_advert_t pub = nullptr;
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if (pub != nullptr) {
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orb_publish(ORB_ID(subsystem_info), pub, &info);
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} else {
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pub = orb_advertise(ORB_ID(subsystem_info), &info);
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}
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publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_SENSORPROXIMITY, true, true, true);
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}
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void
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@ -60,6 +60,7 @@
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#include <perf/perf_counter.h>
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#include <systemlib/err.h>
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#include <systemlib/subsystem_info_pub.h>
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#include <drivers/drv_hrt.h>
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#include <drivers/drv_range_finder.h>
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@ -670,20 +671,7 @@ TERARANGER::start()
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work_queue(HPWORK, &_work, (worker_t)&TERARANGER::cycle_trampoline, this, 1);
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/* notify about state change */
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struct subsystem_info_s info = {};
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info.present = true;
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info.enabled = true;
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info.ok = true;
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info.subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_RANGEFINDER;
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static orb_advert_t pub = nullptr;
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if (pub != nullptr) {
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orb_publish(ORB_ID(subsystem_info), pub, &info);
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} else {
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pub = orb_advertise(ORB_ID(subsystem_info), &info);
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}
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publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_SENSORPROXIMITY, true, true, true);
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}
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void
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@ -61,6 +61,7 @@
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#include <perf/perf_counter.h>
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#include <systemlib/err.h>
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#include <systemlib/subsystem_info_pub.h>
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#include <drivers/drv_hrt.h>
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#include <drivers/drv_range_finder.h>
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@ -609,22 +610,7 @@ TFMINI::start()
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work_queue(HPWORK, &_work, (worker_t)&TFMINI::cycle_trampoline, this, 1);
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/* notify about state change */
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struct subsystem_info_s info = {};
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info.present = true;
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info.enabled = true;
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info.ok = true;
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info.subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_RANGEFINDER;
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static orb_advert_t pub = nullptr;
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if (pub != nullptr) {
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orb_publish(ORB_ID(subsystem_info), pub, &info);
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} else {
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pub = orb_advertise(ORB_ID(subsystem_info), &info);
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}
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publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_SENSORPROXIMITY, true, true, true);
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}
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void
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@ -73,7 +73,6 @@
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#include <uORB/uORB.h>
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#include <uORB/topics/pwm_input.h>
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#include <uORB/topics/subsystem_info.h>
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#include <drivers/drv_device.h>
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#include <drivers/device/device.h>
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@ -65,6 +65,7 @@
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#include <perf/perf_counter.h>
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#include <systemlib/err.h>
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#include <parameters/param.h>
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#include <systemlib/subsystem_info_pub.h>
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#include <conversion/rotation.h>
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@ -589,20 +590,7 @@ PX4FLOW::start()
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work_queue(HPWORK, &_work, (worker_t)&PX4FLOW::cycle_trampoline, this, 1);
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/* notify about state change */
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struct subsystem_info_s info = {};
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info.present = true;
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info.enabled = true;
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info.ok = true;
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info.subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_OPTICALFLOW;
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static orb_advert_t pub = nullptr;
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if (pub != nullptr) {
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orb_publish(ORB_ID(subsystem_info), pub, &info);
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} else {
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pub = orb_advertise(ORB_ID(subsystem_info), &info);
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}
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publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_OPTICALFLOW, true, true, true);
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}
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void
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@ -54,20 +54,17 @@
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#include <uORB/uORB.h>
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#include <uORB/topics/differential_pressure.h>
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#include <uORB/topics/subsystem_info.h>
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#include <drivers/airspeed/airspeed.h>
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Airspeed::Airspeed(int bus, int address, unsigned conversion_interval, const char *path) :
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I2C("Airspeed", path, bus, address, 100000),
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_sensor_ok(false),
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_last_published_sensor_ok(true), /* initialize differently to force publication */
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_measure_ticks(0),
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_collect_phase(false),
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_diff_pres_offset(0.0f),
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_airspeed_pub(nullptr),
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_airspeed_orb_class_instance(-1),
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_subsys_pub(nullptr),
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_class_instance(-1),
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_conversion_interval(conversion_interval),
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_sample_perf(perf_alloc(PC_ELAPSED, "aspd_read")),
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@ -248,33 +245,9 @@ Airspeed::stop()
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work_cancel(HPWORK, &_work);
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}
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void
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Airspeed::update_status()
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{
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if (_sensor_ok != _last_published_sensor_ok) {
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/* notify about state change */
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struct subsystem_info_s info = {};
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info.present = true;
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info.enabled = true;
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info.ok = _sensor_ok;
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info.subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_DIFFPRESSURE;
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if (_subsys_pub != nullptr) {
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orb_publish(ORB_ID(subsystem_info), _subsys_pub, &info);
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} else {
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_subsys_pub = orb_advertise(ORB_ID(subsystem_info), &info);
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}
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_last_published_sensor_ok = _sensor_ok;
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}
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}
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void
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Airspeed::cycle_trampoline(void *arg)
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{
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Airspeed *dev = (Airspeed *)arg;
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dev->cycle();
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dev->update_status();
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}
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@ -43,7 +43,6 @@
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#include <systemlib/airspeed.h>
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#include <perf/perf_counter.h>
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#include <uORB/topics/differential_pressure.h>
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#include <uORB/topics/subsystem_info.h>
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#include <uORB/uORB.h>
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/* Default I2C bus */
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virtual int measure() = 0;
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virtual int collect() = 0;
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/**
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* Update the subsystem status
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*/
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void update_status();
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work_s _work;
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bool _sensor_ok;
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bool _last_published_sensor_ok;
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uint32_t _measure_ticks;
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bool _collect_phase;
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float _diff_pres_offset;
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orb_advert_t _airspeed_pub;
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int _airspeed_orb_class_instance;
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orb_advert_t _subsys_pub;
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int _class_instance;
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unsigned _conversion_interval;
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@ -55,6 +55,7 @@
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#include <parameters/param.h>
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#include <systemlib/rc_check.h>
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#include <systemlib/mavlink_log.h>
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#include <systemlib/subsystem_info_pub.h>
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#include <drivers/drv_hrt.h>
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#include <drivers/drv_mag.h>
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#include <uORB/topics/sensor_preflight.h>
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#include <uORB/topics/system_power.h>
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#include <uORB/topics/vehicle_gps_position.h>
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#include <uORB/topics/subsystem_info.h>
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#include "PreflightCheck.h"
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@ -118,7 +120,9 @@ static int check_calibration(DevHandle &h, const char *param_template, int &devi
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static bool magnometerCheck(orb_advert_t *mavlink_log_pub, unsigned instance, bool optional, int &device_id, bool report_fail)
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{
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bool present = true;
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bool success = true;
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int ret = 0;
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char s[30];
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sprintf(s, "%s%u", MAG_BASE_DEVICE_PATH, instance);
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@ -131,11 +135,12 @@ static bool magnometerCheck(orb_advert_t *mavlink_log_pub, unsigned instance, bo
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mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: NO MAG SENSOR #%u", instance);
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}
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}
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return false;
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present = false;
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success = false;
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goto out;
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}
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int ret = check_calibration(h, "CAL_MAG%u_ID", device_id);
|
||||
ret = check_calibration(h, "CAL_MAG%u_ID", device_id);
|
||||
|
||||
if (ret) {
|
||||
if (report_fail) {
|
||||
|
@ -158,6 +163,9 @@ static bool magnometerCheck(orb_advert_t *mavlink_log_pub, unsigned instance, bo
|
|||
}
|
||||
|
||||
out:
|
||||
if(instance==0) publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_MAG, present, !optional, success);
|
||||
if(instance==1) publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_MAG2, present, !optional, success);
|
||||
|
||||
DevMgr::releaseHandle(h);
|
||||
return success;
|
||||
}
|
||||
|
@ -182,8 +190,9 @@ static bool imuConsistencyCheck(orb_advert_t *mavlink_log_pub, bool report_statu
|
|||
if (sensors.accel_inconsistency_m_s_s > test_limit) {
|
||||
if (report_status) {
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: ACCELS INCONSISTENT - CHECK CAL");
|
||||
publish_subsystem_info_healthy(subsystem_info_s::SUBSYSTEM_TYPE_ACC, false);
|
||||
publish_subsystem_info_healthy(subsystem_info_s::SUBSYSTEM_TYPE_ACC2, false);
|
||||
}
|
||||
|
||||
success = false;
|
||||
goto out;
|
||||
|
||||
|
@ -199,6 +208,8 @@ static bool imuConsistencyCheck(orb_advert_t *mavlink_log_pub, bool report_statu
|
|||
if (sensors.gyro_inconsistency_rad_s > test_limit) {
|
||||
if (report_status) {
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: GYROS INCONSISTENT - CHECK CAL");
|
||||
publish_subsystem_info_healthy(subsystem_info_s::SUBSYSTEM_TYPE_GYRO, false);
|
||||
publish_subsystem_info_healthy(subsystem_info_s::SUBSYSTEM_TYPE_GYRO2, false);
|
||||
}
|
||||
|
||||
success = false;
|
||||
|
@ -238,7 +249,8 @@ static bool magConsistencyCheck(orb_advert_t *mavlink_log_pub, bool report_statu
|
|||
if (report_status) {
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: MAG SENSORS INCONSISTENT");
|
||||
}
|
||||
|
||||
publish_subsystem_info_healthy(subsystem_info_s::SUBSYSTEM_TYPE_MAG, false);
|
||||
publish_subsystem_info_healthy(subsystem_info_s::SUBSYSTEM_TYPE_MAG2, false);
|
||||
return false;
|
||||
}
|
||||
|
||||
|
@ -247,7 +259,9 @@ static bool magConsistencyCheck(orb_advert_t *mavlink_log_pub, bool report_statu
|
|||
|
||||
static bool accelerometerCheck(orb_advert_t *mavlink_log_pub, unsigned instance, bool optional, bool dynamic, int &device_id, bool report_fail)
|
||||
{
|
||||
bool present = true;
|
||||
bool success = true;
|
||||
int ret = 0;
|
||||
|
||||
char s[30];
|
||||
sprintf(s, "%s%u", ACCEL_BASE_DEVICE_PATH, instance);
|
||||
|
@ -260,11 +274,12 @@ static bool accelerometerCheck(orb_advert_t *mavlink_log_pub, unsigned instance,
|
|||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: NO ACCEL SENSOR #%u", instance);
|
||||
}
|
||||
}
|
||||
|
||||
return false;
|
||||
present = false;
|
||||
success = false;
|
||||
goto out;
|
||||
}
|
||||
|
||||
int ret = check_calibration(h, "CAL_ACC%u_ID", device_id);
|
||||
ret = check_calibration(h, "CAL_ACC%u_ID", device_id);
|
||||
|
||||
if (ret) {
|
||||
if (report_fail) {
|
||||
|
@ -321,13 +336,18 @@ static bool accelerometerCheck(orb_advert_t *mavlink_log_pub, unsigned instance,
|
|||
#endif
|
||||
|
||||
out:
|
||||
if(instance==0) publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_ACC, present, !optional, success);
|
||||
if(instance==1) publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_ACC2, present, !optional, success);
|
||||
|
||||
DevMgr::releaseHandle(h);
|
||||
return success;
|
||||
}
|
||||
|
||||
static bool gyroCheck(orb_advert_t *mavlink_log_pub, unsigned instance, bool optional, int &device_id, bool report_fail)
|
||||
{
|
||||
bool present = true;
|
||||
bool success = true;
|
||||
int ret = 0;
|
||||
|
||||
char s[30];
|
||||
sprintf(s, "%s%u", GYRO_BASE_DEVICE_PATH, instance);
|
||||
|
@ -340,11 +360,12 @@ static bool gyroCheck(orb_advert_t *mavlink_log_pub, unsigned instance, bool opt
|
|||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: NO GYRO SENSOR #%u", instance);
|
||||
}
|
||||
}
|
||||
|
||||
return false;
|
||||
present = false;
|
||||
success = false;
|
||||
goto out;
|
||||
}
|
||||
|
||||
int ret = check_calibration(h, "CAL_GYRO%u_ID", device_id);
|
||||
ret = check_calibration(h, "CAL_GYRO%u_ID", device_id);
|
||||
|
||||
if (ret) {
|
||||
if (report_fail) {
|
||||
|
@ -367,6 +388,9 @@ static bool gyroCheck(orb_advert_t *mavlink_log_pub, unsigned instance, bool opt
|
|||
}
|
||||
|
||||
out:
|
||||
if(instance==0) publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_GYRO, present, !optional, success);
|
||||
if(instance==1) publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_GYRO2, present, !optional, success);
|
||||
|
||||
DevMgr::releaseHandle(h);
|
||||
return success;
|
||||
}
|
||||
|
@ -386,7 +410,7 @@ static bool baroCheck(orb_advert_t *mavlink_log_pub, unsigned instance, bool opt
|
|||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: NO BARO SENSOR #%u", instance);
|
||||
}
|
||||
}
|
||||
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_ABSPRESSURE, false, !optional, false);
|
||||
return false;
|
||||
}
|
||||
|
||||
|
@ -402,13 +426,14 @@ static bool baroCheck(orb_advert_t *mavlink_log_pub, unsigned instance, bool opt
|
|||
// }
|
||||
|
||||
//out:
|
||||
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_ABSPRESSURE, true, !optional, success);
|
||||
DevMgr::releaseHandle(h);
|
||||
return success;
|
||||
}
|
||||
|
||||
static bool airspeedCheck(orb_advert_t *mavlink_log_pub, bool optional, bool report_fail, bool prearm)
|
||||
{
|
||||
bool present = true;
|
||||
bool success = true;
|
||||
|
||||
int fd_airspeed = orb_subscribe(ORB_ID(airspeed));
|
||||
|
@ -419,20 +444,20 @@ static bool airspeedCheck(orb_advert_t *mavlink_log_pub, bool optional, bool rep
|
|||
|
||||
if ((orb_copy(ORB_ID(differential_pressure), fd_diffpres, &differential_pressure) != PX4_OK) ||
|
||||
(hrt_elapsed_time(&differential_pressure.timestamp) > 1000000)) {
|
||||
if (report_fail) {
|
||||
if (report_fail && !optional) {
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: AIRSPEED SENSOR MISSING");
|
||||
}
|
||||
|
||||
present = false;
|
||||
success = false;
|
||||
goto out;
|
||||
}
|
||||
|
||||
if ((orb_copy(ORB_ID(airspeed), fd_airspeed, &airspeed) != PX4_OK) ||
|
||||
(hrt_elapsed_time(&airspeed.timestamp) > 1000000)) {
|
||||
if (report_fail) {
|
||||
if (report_fail && !optional) {
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: AIRSPEED SENSOR MISSING");
|
||||
}
|
||||
|
||||
present = false;
|
||||
success = false;
|
||||
goto out;
|
||||
}
|
||||
|
@ -447,7 +472,7 @@ static bool airspeedCheck(orb_advert_t *mavlink_log_pub, bool optional, bool rep
|
|||
if (report_fail) {
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: AIRSPEED SENSOR STUCK");
|
||||
}
|
||||
|
||||
present = true;
|
||||
success = false;
|
||||
goto out;
|
||||
}
|
||||
|
@ -461,12 +486,13 @@ static bool airspeedCheck(orb_advert_t *mavlink_log_pub, bool optional, bool rep
|
|||
if (report_fail) {
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: CHECK AIRSPEED CAL OR PITOT");
|
||||
}
|
||||
|
||||
present = true;
|
||||
success = false;
|
||||
goto out;
|
||||
}
|
||||
|
||||
out:
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_DIFFPRESSURE, present, !optional, success);
|
||||
orb_unsubscribe(fd_airspeed);
|
||||
orb_unsubscribe(fd_diffpres);
|
||||
return success;
|
||||
|
@ -523,6 +549,7 @@ static bool powerCheck(orb_advert_t *mavlink_log_pub, bool report_fail, bool pre
|
|||
static bool ekf2Check(orb_advert_t *mavlink_log_pub, bool optional, bool report_fail, bool enforce_gps_required)
|
||||
{
|
||||
bool success = true; // start with a pass and change to a fail if any test fails
|
||||
bool present = true;
|
||||
float test_limit = 1.0f; // pass limit re-used for each test
|
||||
|
||||
// Get estimator status data if available and exit with a fail recorded if not
|
||||
|
@ -530,6 +557,7 @@ static bool ekf2Check(orb_advert_t *mavlink_log_pub, bool optional, bool report_
|
|||
estimator_status_s status = {};
|
||||
|
||||
if (orb_copy(ORB_ID(estimator_status), sub, &status) != PX4_OK) {
|
||||
present = false;
|
||||
goto out;
|
||||
}
|
||||
|
||||
|
@ -626,12 +654,13 @@ static bool ekf2Check(orb_advert_t *mavlink_log_pub, bool optional, bool report_
|
|||
// The EKF is not using GPS
|
||||
if (report_fail) {
|
||||
if (ekf_gps_check_fail) {
|
||||
// Poor GPS qulaity is the likely cause
|
||||
// Poor GPS quality is the likely cause
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: GPS QUALITY POOR");
|
||||
|
||||
publish_subsystem_info_healthy(subsystem_info_s::SUBSYSTEM_TYPE_GPS, false);
|
||||
} else {
|
||||
// Likely cause unknown
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: EKF NOT USING GPS");
|
||||
publish_subsystem_info_healthy(subsystem_info_s::SUBSYSTEM_TYPE_GPS, false);
|
||||
}
|
||||
}
|
||||
|
||||
|
@ -649,6 +678,7 @@ static bool ekf2Check(orb_advert_t *mavlink_log_pub, bool optional, bool report_
|
|||
if (gps_quality_fail) {
|
||||
if (report_fail) {
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: GPS QUALITY POOR");
|
||||
publish_subsystem_info_healthy(subsystem_info_s::SUBSYSTEM_TYPE_GPS, false);
|
||||
}
|
||||
|
||||
success = false;
|
||||
|
@ -658,15 +688,15 @@ static bool ekf2Check(orb_advert_t *mavlink_log_pub, bool optional, bool report_
|
|||
}
|
||||
|
||||
out:
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_AHRS, present, !optional, success && present);
|
||||
orb_unsubscribe(sub);
|
||||
return success;
|
||||
}
|
||||
|
||||
bool preflightCheck(orb_advert_t *mavlink_log_pub, const vehicle_status_s &status,
|
||||
const vehicle_status_flags_s &status_flags, bool checkGNSS, bool reportFailures, bool prearm,
|
||||
vehicle_status_flags_s &status_flags, bool checkGNSS, bool reportFailures, bool prearm,
|
||||
const hrt_abstime &time_since_boot)
|
||||
{
|
||||
|
||||
if (time_since_boot < 2000000) {
|
||||
// the airspeed driver filter doesn't deliver the actual value yet
|
||||
reportFailures = false;
|
||||
|
@ -737,7 +767,7 @@ bool preflightCheck(orb_advert_t *mavlink_log_pub, const vehicle_status_s &statu
|
|||
if ((reportFailures && !failed)) {
|
||||
mavlink_log_critical(mavlink_log_pub, "Primary compass not found");
|
||||
}
|
||||
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_MAG, false, true, false);
|
||||
failed = true;
|
||||
}
|
||||
|
||||
|
@ -775,7 +805,7 @@ bool preflightCheck(orb_advert_t *mavlink_log_pub, const vehicle_status_s &statu
|
|||
if ((reportFailures && !failed)) {
|
||||
mavlink_log_critical(mavlink_log_pub, "Primary accelerometer not found");
|
||||
}
|
||||
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_ACC, false, true, false);
|
||||
failed = true;
|
||||
}
|
||||
}
|
||||
|
@ -808,7 +838,7 @@ bool preflightCheck(orb_advert_t *mavlink_log_pub, const vehicle_status_s &statu
|
|||
if ((reportFailures && !failed)) {
|
||||
mavlink_log_critical(mavlink_log_pub, "Primary gyro not found");
|
||||
}
|
||||
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_GYRO, false, true, false);
|
||||
failed = true;
|
||||
}
|
||||
}
|
||||
|
@ -844,7 +874,7 @@ bool preflightCheck(orb_advert_t *mavlink_log_pub, const vehicle_status_s &statu
|
|||
if (reportFailures && !failed) {
|
||||
mavlink_log_critical(mavlink_log_pub, "Primary barometer not operational");
|
||||
}
|
||||
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_ABSPRESSURE, false, true, false);
|
||||
failed = true;
|
||||
}
|
||||
}
|
||||
|
@ -858,7 +888,10 @@ bool preflightCheck(orb_advert_t *mavlink_log_pub, const vehicle_status_s &statu
|
|||
|
||||
/* ---- AIRSPEED ---- */
|
||||
if (checkAirspeed) {
|
||||
if (!airspeedCheck(mavlink_log_pub, true, reportFailures && !failed, prearm)) {
|
||||
int32_t optional = 0; //Given checkAirspeed==true, assume the airspeed sensor is also required by default
|
||||
param_get(param_find("FW_ARSP_MODE"), &optional);
|
||||
|
||||
if (!airspeedCheck(mavlink_log_pub, (bool)optional, reportFailures && !failed, prearm) && !(bool)optional) {
|
||||
failed = true;
|
||||
}
|
||||
}
|
||||
|
@ -871,6 +904,13 @@ bool preflightCheck(orb_advert_t *mavlink_log_pub, const vehicle_status_s &statu
|
|||
}
|
||||
|
||||
failed = true;
|
||||
|
||||
publish_subsystem_info_enabled_healthy(subsystem_info_s::SUBSYSTEM_TYPE_RCRECEIVER, true, false);
|
||||
status_flags.rc_calibration_valid = false;
|
||||
} else {
|
||||
// The calibration is fine, but only set the overall health state to true if the signal is not currently lost
|
||||
status_flags.rc_calibration_valid = true;
|
||||
publish_subsystem_info_enabled_healthy(subsystem_info_s::SUBSYSTEM_TYPE_RCRECEIVER, true, !status.rc_signal_lost);
|
||||
}
|
||||
}
|
||||
|
||||
|
@ -881,6 +921,29 @@ bool preflightCheck(orb_advert_t *mavlink_log_pub, const vehicle_status_s &statu
|
|||
}
|
||||
}
|
||||
|
||||
/* ---- GPS ---- */
|
||||
if (checkGNSS) {
|
||||
int fd_gps = orb_subscribe(ORB_ID(vehicle_gps_position));
|
||||
vehicle_gps_position_s gps = {};
|
||||
bool present = true;
|
||||
|
||||
if ((orb_copy(ORB_ID(vehicle_gps_position), fd_gps, &gps) != PX4_OK) ||
|
||||
(hrt_elapsed_time(&gps.timestamp) > 2000000)) {
|
||||
if (reportFailures) {
|
||||
mavlink_log_critical(mavlink_log_pub, "PREFLIGHT FAIL: GPS MODULE MISSING");
|
||||
}
|
||||
present = false;
|
||||
}
|
||||
|
||||
// Mark GPS as required (given that checkGNSS=true) and indicate whether it is present. For now also assume it is healthy
|
||||
// if there is a lock ... EKF2 will then set the healthy=false if its more extensive GPS checks fail in the next step.
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_GPS, present, true, present && gps.fix_type>=3);
|
||||
}
|
||||
|
||||
// TODO: Add rangefinder here. We have the SENS_EN_XXX params that tell us what we should have. This is currently completely done inside the driver.
|
||||
|
||||
// TODO: Add optical flow check here? This is currently completely done inside the driver.
|
||||
|
||||
/* ---- Navigation EKF ---- */
|
||||
// only check EKF2 data if EKF2 is selected as the estimator and GNSS checking is enabled
|
||||
int32_t estimator_type;
|
||||
|
@ -889,8 +952,7 @@ bool preflightCheck(orb_advert_t *mavlink_log_pub, const vehicle_status_s &statu
|
|||
if (estimator_type == 2) {
|
||||
// don't report ekf failures for the first 10 seconds to allow time for the filter to start
|
||||
bool report_ekf_fail = (time_since_boot > 10 * 1000000);
|
||||
|
||||
if (!ekf2Check(mavlink_log_pub, true, (reportFailures && report_ekf_fail && !failed), checkGNSS)) {
|
||||
if (!ekf2Check(mavlink_log_pub, false, reportFailures && report_ekf_fail && !failed, checkGNSS)) {
|
||||
failed = true;
|
||||
}
|
||||
}
|
||||
|
|
|
@ -43,6 +43,8 @@
|
|||
#include <uORB/topics/vehicle_status.h>
|
||||
#include <uORB/topics/vehicle_status_flags.h>
|
||||
|
||||
#include <uORB/topics/vehicle_status_flags.h>
|
||||
|
||||
#pragma once
|
||||
|
||||
namespace Preflight
|
||||
|
@ -73,7 +75,7 @@ namespace Preflight
|
|||
* true if the system power should be checked
|
||||
**/
|
||||
bool preflightCheck(orb_advert_t *mavlink_log_pub, const vehicle_status_s &status,
|
||||
const vehicle_status_flags_s &status_flags, bool checkGNSS, bool reportFailures, bool prearm,
|
||||
vehicle_status_flags_s &status_flags, bool checkGNSS, bool reportFailures, bool prearm,
|
||||
const hrt_abstime &time_since_boot);
|
||||
|
||||
static constexpr unsigned max_mandatory_gyro_count = 1;
|
||||
|
|
|
@ -79,6 +79,7 @@
|
|||
#include <parameters/param.h>
|
||||
#include <systemlib/rc_check.h>
|
||||
#include <systemlib/state_table.h>
|
||||
#include <systemlib/subsystem_info_pub.h>
|
||||
|
||||
#include <cmath>
|
||||
#include <cfloat>
|
||||
|
@ -1256,6 +1257,7 @@ Commander::run()
|
|||
|
||||
status_flags.condition_power_input_valid = true;
|
||||
status_flags.usb_connected = false;
|
||||
status_flags.rc_calibration_valid = true;
|
||||
|
||||
// CIRCUIT BREAKERS
|
||||
status_flags.circuit_breaker_engaged_power_check = false;
|
||||
|
@ -1270,6 +1272,11 @@ Commander::run()
|
|||
status_flags.condition_local_velocity_valid = false;
|
||||
status_flags.condition_local_altitude_valid = false;
|
||||
|
||||
bool status_changed = true;
|
||||
|
||||
/* initialize the vehicle status flag helper functions. This also initializes the sensor health flags*/
|
||||
publish_subsystem_info_init(&status, &status_changed);
|
||||
|
||||
/* publish initial state */
|
||||
status_pub = orb_advertise(ORB_ID(vehicle_status), &status);
|
||||
|
||||
|
@ -1310,7 +1317,6 @@ Commander::run()
|
|||
bool emergency_battery_voltage_actions_done = false;
|
||||
bool dangerous_battery_level_requests_poweroff = false;
|
||||
|
||||
bool status_changed = true;
|
||||
bool param_init_forced = true;
|
||||
|
||||
bool updated = false;
|
||||
|
@ -1825,6 +1831,12 @@ Commander::run()
|
|||
}
|
||||
}
|
||||
|
||||
if((_last_condition_global_position_valid != status_flags.condition_global_position_valid) && status_flags.condition_global_position_valid) {
|
||||
// If global position state changed and is now valid, set respective health flags to true. For now also assume GPS is OK if global pos is OK, but not vice versa.
|
||||
publish_subsystem_info_healthy(subsystem_info_s::SUBSYSTEM_TYPE_AHRS, true);
|
||||
publish_subsystem_info_present_healthy(subsystem_info_s::SUBSYSTEM_TYPE_GPS, true, true);
|
||||
}
|
||||
|
||||
check_valid(_local_position_sub.get().timestamp, _failsafe_pos_delay.get() * 1_s, _local_position_sub.get().z_valid, &(status_flags.condition_local_altitude_valid), &status_changed);
|
||||
|
||||
/* Update land detector */
|
||||
|
@ -1993,41 +2005,6 @@ Commander::run()
|
|||
}
|
||||
}
|
||||
|
||||
/* update subsystem */
|
||||
orb_check(subsys_sub, &updated);
|
||||
|
||||
if (updated) {
|
||||
orb_copy(ORB_ID(subsystem_info), subsys_sub, &info);
|
||||
|
||||
//warnx("subsystem changed: %d\n", (int)info.subsystem_type);
|
||||
|
||||
/* mark / unmark as present */
|
||||
if (info.present) {
|
||||
status.onboard_control_sensors_present |= info.subsystem_type;
|
||||
|
||||
} else {
|
||||
status.onboard_control_sensors_present &= ~info.subsystem_type;
|
||||
}
|
||||
|
||||
/* mark / unmark as enabled */
|
||||
if (info.enabled) {
|
||||
status.onboard_control_sensors_enabled |= info.subsystem_type;
|
||||
|
||||
} else {
|
||||
status.onboard_control_sensors_enabled &= ~info.subsystem_type;
|
||||
}
|
||||
|
||||
/* mark / unmark as ok */
|
||||
if (info.ok) {
|
||||
status.onboard_control_sensors_health |= info.subsystem_type;
|
||||
|
||||
} else {
|
||||
status.onboard_control_sensors_health &= ~info.subsystem_type;
|
||||
}
|
||||
|
||||
status_changed = true;
|
||||
}
|
||||
|
||||
/* If in INIT state, try to proceed to STANDBY state */
|
||||
if (!status_flags.condition_calibration_enabled && status.arming_state == vehicle_status_s::ARMING_STATE_INIT) {
|
||||
|
||||
|
@ -2223,11 +2200,13 @@ Commander::run()
|
|||
/* handle the case where RC signal was regained */
|
||||
if (!status_flags.rc_signal_found_once) {
|
||||
status_flags.rc_signal_found_once = true;
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_RCRECEIVER, true, true, true && status_flags.rc_calibration_valid);
|
||||
status_changed = true;
|
||||
|
||||
} else {
|
||||
if (status.rc_signal_lost) {
|
||||
mavlink_log_info(&mavlink_log_pub, "MANUAL CONTROL REGAINED after %llums", hrt_elapsed_time(&rc_signal_lost_timestamp) / 1000);
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_RCRECEIVER, true, true, true && status_flags.rc_calibration_valid);
|
||||
status_changed = true;
|
||||
}
|
||||
}
|
||||
|
@ -2375,6 +2354,7 @@ Commander::run()
|
|||
mavlink_log_critical(&mavlink_log_pub, "MANUAL CONTROL LOST (at t=%llums)", hrt_absolute_time() / 1000);
|
||||
status.rc_signal_lost = true;
|
||||
rc_signal_lost_timestamp = sp_man.timestamp;
|
||||
publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_RCRECEIVER, true, true, false);
|
||||
status_changed = true;
|
||||
}
|
||||
}
|
||||
|
@ -4096,6 +4076,9 @@ void Commander::poll_telemetry_status()
|
|||
(mission_result.instance_count > 0) && !mission_result.valid) {
|
||||
|
||||
mavlink_log_critical(&mavlink_log_pub, "Planned mission fails check. Please upload again.");
|
||||
//publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_MISSION, true, true, false); // TODO
|
||||
} else {
|
||||
//publish_subsystem_info(subsystem_info_s::SUBSYSTEM_TYPE_MISSION, true, true, true); // TODO
|
||||
}
|
||||
}
|
||||
|
||||
|
|
|
@ -40,6 +40,7 @@
|
|||
#include "voted_sensors_update.h"
|
||||
|
||||
#include <systemlib/mavlink_log.h>
|
||||
#include <systemlib/subsystem_info_pub.h>
|
||||
|
||||
#include <conversion/rotation.h>
|
||||
#include <ecl/geo/geo.h>
|
||||
|
@ -897,18 +898,15 @@ bool VotedSensorsUpdate::check_failover(SensorData &sensor, const char *sensor_n
|
|||
if (sensor.last_failover_count != sensor.voter.failover_count()) {
|
||||
|
||||
uint32_t flags = sensor.voter.failover_state();
|
||||
|
||||
if (flags == DataValidator::ERROR_FLAG_NO_ERROR) {
|
||||
int failover_index = sensor.voter.failover_index();
|
||||
|
||||
if (flags == DataValidator::ERROR_FLAG_NO_ERROR) {
|
||||
if (failover_index != -1) {
|
||||
//we switched due to a non-critical reason. No need to panic.
|
||||
PX4_INFO("%s sensor switch from #%i", sensor_name, failover_index);
|
||||
}
|
||||
|
||||
} else {
|
||||
int failover_index = sensor.voter.failover_index();
|
||||
|
||||
if (failover_index != -1) {
|
||||
mavlink_log_emergency(&_mavlink_log_pub, "%s #%i fail: %s%s%s%s%s!",
|
||||
sensor_name,
|
||||
|
@ -921,6 +919,40 @@ bool VotedSensorsUpdate::check_failover(SensorData &sensor, const char *sensor_n
|
|||
|
||||
// reduce priority of failed sensor to the minimum
|
||||
sensor.priority[failover_index] = 1;
|
||||
|
||||
// Update the subsystem_info uORB given that a sensor failed
|
||||
int ctr_valid = 0;
|
||||
|
||||
for (uint8_t i = 0; i < sensor.subscription_count; i++) {
|
||||
if (sensor.priority[i] > 1) { ctr_valid++; }
|
||||
|
||||
PX4_WARN("FAILOVER event (idx=%u)! Sensor %s: Nr. %u Priority: %u", failover_index, sensor_name, i, sensor.priority[i]);
|
||||
}
|
||||
|
||||
PX4_INFO("%s sensor switch from #%i", sensor_name, failover_index);
|
||||
|
||||
if (ctr_valid < 2) { // subsystem_info only contains flags for the first two sensors
|
||||
uint64_t subsystem_type = 0;
|
||||
|
||||
if (ctr_valid == 0) { // There are no valid sensors left!
|
||||
if (strcmp(sensor_name, "Gyro") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_GYRO; }
|
||||
|
||||
if (strcmp(sensor_name, "Accel") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_ACC; }
|
||||
|
||||
if (strcmp(sensor_name, "Mag") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_MAG; }
|
||||
|
||||
if (strcmp(sensor_name, "Baro") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_ABSPRESSURE; }
|
||||
|
||||
} else if (ctr_valid == 1) { // A single valid sensor remains, set secondary sensor health to false
|
||||
if (strcmp(sensor_name, "Gyro") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_GYRO2; }
|
||||
|
||||
if (strcmp(sensor_name, "Accel") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_ACC2; }
|
||||
|
||||
if (strcmp(sensor_name, "Mag") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_MAG2; }
|
||||
}
|
||||
|
||||
publish_subsystem_info_healthy(subsystem_type, false);
|
||||
}
|
||||
}
|
||||
}
|
||||
|
||||
|
@ -951,6 +983,30 @@ void VotedSensorsUpdate::init_sensor_class(const struct orb_metadata *meta, Sens
|
|||
PX4_ERR("failed to add validator for sensor %s %i", meta->o_name, i);
|
||||
}
|
||||
}
|
||||
|
||||
// Update the subsystem_info uORB to indicate the amount of valid sensors
|
||||
if (i < 2) { // subsystem_info only contains flags for the first two sensors
|
||||
uint64_t subsystem_type = 0;
|
||||
|
||||
if (i == 0) { // First sensor valid
|
||||
if (strcmp(meta->o_name, "sensor_gyro") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_GYRO; }
|
||||
|
||||
if (strcmp(meta->o_name, "sensor_accel") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_ACC; }
|
||||
|
||||
if (strcmp(meta->o_name, "sensor_mag") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_MAG; }
|
||||
|
||||
if (strcmp(meta->o_name, "sensor_baro") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_ABSPRESSURE; }
|
||||
|
||||
} else if (i == 1) { // We also have a second sensor
|
||||
if (strcmp(meta->o_name, "sensor_gyro") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_GYRO2; }
|
||||
|
||||
if (strcmp(meta->o_name, "sensor_accel") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_ACC2; }
|
||||
|
||||
if (strcmp(meta->o_name, "sensor_mag") == 0) { subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_MAG2; }
|
||||
}
|
||||
|
||||
publish_subsystem_info(subsystem_type, true, true, true);
|
||||
}
|
||||
}
|
||||
}
|
||||
|
||||
|
|
|
@ -58,6 +58,7 @@
|
|||
#include <uORB/topics/sensor_selection.h>
|
||||
#include <uORB/topics/vehicle_air_data.h>
|
||||
#include <uORB/topics/vehicle_magnetometer.h>
|
||||
#include <uORB/topics/subsystem_info.h>
|
||||
|
||||
#include <DevMgr.hpp>
|
||||
|
||||
|
|
|
@ -65,7 +65,6 @@
|
|||
|
||||
#include <uORB/uORB.h>
|
||||
#include <uORB/topics/differential_pressure.h>
|
||||
#include <uORB/topics/subsystem_info.h>
|
||||
|
||||
#include <simulator/simulator.h>
|
||||
|
||||
|
@ -76,12 +75,10 @@ AirspeedSim::AirspeedSim(int bus, int address, unsigned conversion_interval, con
|
|||
_reports(nullptr),
|
||||
_retries(0),
|
||||
_sensor_ok(false),
|
||||
_last_published_sensor_ok(true), /* initialize differently to force publication */
|
||||
_measure_ticks(0),
|
||||
_collect_phase(false),
|
||||
_diff_pres_offset(0.0f),
|
||||
_airspeed_pub(nullptr),
|
||||
_subsys_pub(nullptr),
|
||||
_class_instance(-1),
|
||||
_conversion_interval(conversion_interval),
|
||||
_sample_perf(perf_alloc(PC_ELAPSED, "airspeed_read")),
|
||||
|
@ -360,38 +357,12 @@ AirspeedSim::stop()
|
|||
work_cancel(HPWORK, &_work);
|
||||
}
|
||||
|
||||
void
|
||||
AirspeedSim::update_status()
|
||||
{
|
||||
if (_sensor_ok != _last_published_sensor_ok) {
|
||||
/* notify about state change */
|
||||
struct subsystem_info_s info = {};
|
||||
info.present = true;
|
||||
info.enabled = true;
|
||||
info.ok = _sensor_ok;
|
||||
info.subsystem_type = subsystem_info_s::SUBSYSTEM_TYPE_DIFFPRESSURE;
|
||||
|
||||
if (_subsys_pub != nullptr) {
|
||||
orb_publish(ORB_ID(subsystem_info), _subsys_pub, &info);
|
||||
|
||||
} else {
|
||||
_subsys_pub = orb_advertise(ORB_ID(subsystem_info), &info);
|
||||
}
|
||||
|
||||
_last_published_sensor_ok = _sensor_ok;
|
||||
}
|
||||
}
|
||||
|
||||
void
|
||||
AirspeedSim::cycle_trampoline(void *arg)
|
||||
{
|
||||
AirspeedSim *dev = (AirspeedSim *)arg;
|
||||
|
||||
dev->cycle();
|
||||
// XXX we do not know if this is
|
||||
// really helping - do not update the
|
||||
// subsys state right now
|
||||
//dev->update_status();
|
||||
}
|
||||
|
||||
void
|
||||
|
|
|
@ -69,7 +69,6 @@
|
|||
|
||||
#include <uORB/uORB.h>
|
||||
#include <uORB/topics/differential_pressure.h>
|
||||
#include <uORB/topics/subsystem_info.h>
|
||||
|
||||
/* Default I2C bus */
|
||||
#define PX4_I2C_BUS_DEFAULT PX4_I2C_BUS_EXPANSION
|
||||
|
@ -117,20 +116,13 @@ protected:
|
|||
virtual int transfer(const uint8_t *send, unsigned send_len,
|
||||
uint8_t *recv, unsigned recv_len);
|
||||
|
||||
/**
|
||||
* Update the subsystem status
|
||||
*/
|
||||
void update_status();
|
||||
|
||||
struct work_s _work;
|
||||
bool _sensor_ok;
|
||||
bool _last_published_sensor_ok;
|
||||
unsigned _measure_ticks;
|
||||
bool _collect_phase;
|
||||
float _diff_pres_offset;
|
||||
|
||||
orb_advert_t _airspeed_pub;
|
||||
orb_advert_t _subsys_pub;
|
||||
|
||||
int _class_instance;
|
||||
|
||||
|
|
|
@ -71,7 +71,6 @@
|
|||
|
||||
#include <uORB/uORB.h>
|
||||
#include <uORB/topics/differential_pressure.h>
|
||||
#include <uORB/topics/subsystem_info.h>
|
||||
#include <uORB/topics/system_power.h>
|
||||
|
||||
#include "airspeedsim.h"
|
||||
|
|
|
@ -44,6 +44,7 @@ set(SRCS
|
|||
pid/pid.c
|
||||
pwm_limit/pwm_limit.c
|
||||
rc_check.c
|
||||
subsystem_info_pub.cpp
|
||||
)
|
||||
|
||||
if(${OS} STREQUAL "nuttx")
|
||||
|
|
|
@ -0,0 +1,148 @@
|
|||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2013 PX4 Development Team. All rights reserved.
|
||||
*
|
||||
* Redistribution and use in source and binary forms, with or without
|
||||
* modification, are permitted provided that the following conditions
|
||||
* are met:
|
||||
*
|
||||
* 1. Redistributions of source code must retain the above copyright
|
||||
* notice, this list of conditions and the following disclaimer.
|
||||
* 2. Redistributions in binary form must reproduce the above copyright
|
||||
* notice, this list of conditions and the following disclaimer in
|
||||
* the documentation and/or other materials provided with the
|
||||
* distribution.
|
||||
* 3. Neither the name PX4 nor the names of its contributors may be
|
||||
* used to endorse or promote products derived from this software
|
||||
* without specific prior written permission.
|
||||
*
|
||||
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||
* POSSIBILITY OF SUCH DAMAGE.
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
/**
|
||||
* @file subsystem_info_pub.cpp
|
||||
*
|
||||
* Contains helper functions to efficiently publish the subsystem_info messages from various locations inside the code. It is basically a
|
||||
* helper function for commander. Approach:
|
||||
* - Before commander starts (which happens after some of the drivers have already published the respective subsystem_info), this helper
|
||||
* code stores all requests for a publish_subsystem_info in the internal_status variable
|
||||
* - When commander starts up, it calls the publish_subsystem_info_init function. This 1) copies the internal_status into commander's
|
||||
* vehicle status variable and 2) assigns the status pointer to commanders vehicle status
|
||||
* - After that, all requests to publish_subsystem_info are directly written to commander's vehicle status such that it is always up
|
||||
* to date. Commander then publishes the vehicle_status uORB (and is in fact the only app that does that, which is why this approach works)
|
||||
*
|
||||
* @author Philipp Oettershagen (philipp.oettershagen@mavt.ethz.ch)
|
||||
*/
|
||||
|
||||
#include "subsystem_info_pub.h"
|
||||
|
||||
vehicle_status_s internal_status = {};
|
||||
vehicle_status_s *status = &internal_status;
|
||||
bool *status_changed = nullptr;
|
||||
|
||||
/* initialize pointer to commander's vehicle status variable */
|
||||
void publish_subsystem_info_init(vehicle_status_s *commander_vehicle_status_ptr, bool *commander_status_changed_ptr)
|
||||
{
|
||||
status = commander_vehicle_status_ptr;
|
||||
status_changed = commander_status_changed_ptr;
|
||||
|
||||
status->onboard_control_sensors_present = internal_status.onboard_control_sensors_present;
|
||||
status->onboard_control_sensors_enabled = internal_status.onboard_control_sensors_enabled;
|
||||
status->onboard_control_sensors_health = internal_status.onboard_control_sensors_health;
|
||||
*status_changed = true;
|
||||
}
|
||||
|
||||
/* Writes the full state information for a specific subsystem type, either directly into commander's vehicle
|
||||
* status variable or into an internal variable that is later copied to commander's vehicle status variable*/
|
||||
void publish_subsystem_info(uint64_t subsystem_type, bool present, bool enabled, bool ok)
|
||||
{
|
||||
PX4_DEBUG("publish_subsystem_info (ext:%u): Type %llu pres=%u enabl=%u ok=%u", status != &internal_status,
|
||||
subsystem_type, present, enabled, ok);
|
||||
|
||||
if (present) {
|
||||
status->onboard_control_sensors_present |= (uint32_t)subsystem_type;
|
||||
|
||||
} else {
|
||||
status->onboard_control_sensors_present &= ~(uint32_t)subsystem_type;
|
||||
}
|
||||
|
||||
if (enabled) {
|
||||
status->onboard_control_sensors_enabled |= (uint32_t)subsystem_type;
|
||||
|
||||
} else {
|
||||
status->onboard_control_sensors_enabled &= ~(uint32_t)subsystem_type;
|
||||
}
|
||||
|
||||
if (ok) {
|
||||
status->onboard_control_sensors_health |= (uint32_t)subsystem_type;
|
||||
|
||||
} else {
|
||||
status->onboard_control_sensors_health &= ~(uint32_t)subsystem_type;
|
||||
}
|
||||
|
||||
if (status != &internal_status) { *status_changed = true; }
|
||||
}
|
||||
|
||||
void publish_subsystem_info_present_healthy(uint64_t subsystem_type, bool present, bool healthy)
|
||||
{
|
||||
publish_subsystem_info(subsystem_type, present, getEnabled(subsystem_type), healthy);
|
||||
}
|
||||
|
||||
void publish_subsystem_info_present_enabled(uint64_t subsystem_type, bool present, bool enabled)
|
||||
{
|
||||
publish_subsystem_info(subsystem_type, present, enabled, getHealthy(subsystem_type));
|
||||
}
|
||||
|
||||
void publish_subsystem_info_enabled_healthy(uint64_t subsystem_type, bool enabled, bool ok)
|
||||
{
|
||||
publish_subsystem_info(subsystem_type, getPresent(subsystem_type), enabled, ok);
|
||||
}
|
||||
|
||||
void publish_subsystem_info_enabled(uint64_t subsystem_type, bool enabled)
|
||||
{
|
||||
publish_subsystem_info(subsystem_type, getPresent(subsystem_type), enabled, getHealthy(subsystem_type));
|
||||
}
|
||||
|
||||
void publish_subsystem_info_healthy(uint64_t subsystem_type, bool ok)
|
||||
{
|
||||
publish_subsystem_info(subsystem_type, getPresent(subsystem_type), getEnabled(subsystem_type), ok);
|
||||
}
|
||||
|
||||
void publish_subsystem_info_print()
|
||||
{
|
||||
uint64_t type = 1;
|
||||
|
||||
for (int i = 1; i < 31; i++) {
|
||||
PX4_DEBUG("subsystem_info: Type %llu pres=%u enabl=%u ok=%u", type,
|
||||
(status->onboard_control_sensors_present & (uint32_t)type) > 0,
|
||||
(status->onboard_control_sensors_enabled & (uint32_t)type) > 0,
|
||||
(status->onboard_control_sensors_health & (uint32_t)type) > 0);
|
||||
type = type * 2;
|
||||
}
|
||||
}
|
||||
|
||||
// Local helper functions
|
||||
bool getPresent(uint64_t subsystem_type)
|
||||
{
|
||||
return status->onboard_control_sensors_present & (uint32_t)subsystem_type;
|
||||
}
|
||||
bool getEnabled(uint64_t subsystem_type)
|
||||
{
|
||||
return status->onboard_control_sensors_enabled & (uint32_t)subsystem_type;
|
||||
}
|
||||
bool getHealthy(uint64_t subsystem_type)
|
||||
{
|
||||
return status->onboard_control_sensors_health & (uint32_t)subsystem_type;
|
||||
}
|
|
@ -0,0 +1,62 @@
|
|||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2013 PX4 Development Team. All rights reserved.
|
||||
*
|
||||
* Redistribution and use in source and binary forms, with or without
|
||||
* modification, are permitted provided that the following conditions
|
||||
* are met:
|
||||
*
|
||||
* 1. Redistributions of source code must retain the above copyright
|
||||
* notice, this list of conditions and the following disclaimer.
|
||||
* 2. Redistributions in binary form must reproduce the above copyright
|
||||
* notice, this list of conditions and the following disclaimer in
|
||||
* the documentation and/or other materials provided with the
|
||||
* distribution.
|
||||
* 3. Neither the name PX4 nor the names of its contributors may be
|
||||
* used to endorse or promote products derived from this software
|
||||
* without specific prior written permission.
|
||||
*
|
||||
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||
* POSSIBILITY OF SUCH DAMAGE.
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
/**
|
||||
* @file subsystem_info_pub.h
|
||||
*
|
||||
* Contains helper functions to efficiently publish the subsystem_info topic from various locations inside the code.
|
||||
*
|
||||
* @author Philipp Oettershagen (philipp.oettershagen@mavt.ethz.ch)
|
||||
*/
|
||||
|
||||
#pragma once
|
||||
|
||||
#include <px4_log.h>
|
||||
#include <uORB/uORB.h>
|
||||
#include <uORB/topics/vehicle_status.h>
|
||||
|
||||
void publish_subsystem_info_init(vehicle_status_s *commander_vehicle_status_ptr, bool *commander_status_changed_ptr);
|
||||
void publish_subsystem_info(uint64_t subsystem_type, bool present, bool enabled, bool ok);
|
||||
|
||||
void publish_subsystem_info_present_healthy(uint64_t subsystem_type, bool present, bool healthy);
|
||||
void publish_subsystem_info_present_enabled(uint64_t subsystem_type, bool present, bool enabled);
|
||||
void publish_subsystem_info_enabled_healthy(uint64_t subsystem_type, bool enabled, bool ok);
|
||||
void publish_subsystem_info_enabled(uint64_t subsystem_type, bool enabled);
|
||||
void publish_subsystem_info_healthy(uint64_t subsystem_type, bool ok);
|
||||
|
||||
void publish_subsystem_info_print();
|
||||
|
||||
// Local helper functions
|
||||
bool getPresent(uint64_t subsystem_type);
|
||||
bool getEnabled(uint64_t subsystem_type);
|
||||
bool getHealthy(uint64_t subsystem_type);
|
|
@ -148,9 +148,14 @@ uORB::DeviceNode::open(device::file_t *filp)
|
|||
return -ENOMEM;
|
||||
}
|
||||
|
||||
/* default to no pending update */
|
||||
/* If queue size >1, allow the subscriber to read the data in the queue. Otherwise, assume subscriber is up to date.*/
|
||||
if (_queue_size <= 1) {
|
||||
sd->generation = _generation;
|
||||
|
||||
} else {
|
||||
sd->generation = _generation - (_queue_size < _generation ? _queue_size : _generation);
|
||||
}
|
||||
|
||||
/* set priority */
|
||||
sd->set_priority(_priority);
|
||||
|
||||
|
|
|
@ -57,7 +57,6 @@
|
|||
#include <drivers/drv_hrt.h>
|
||||
|
||||
#include <uORB/uORB.h>
|
||||
#include <uORB/topics/subsystem_info.h>
|
||||
#include <uORB/topics/distance_sensor.h>
|
||||
|
||||
#include <board_config.h>
|
||||
|
|
|
@ -60,7 +60,6 @@
|
|||
#include <drivers/drv_hrt.h>
|
||||
|
||||
#include <uORB/uORB.h>
|
||||
#include <uORB/topics/subsystem_info.h>
|
||||
#include <uORB/topics/distance_sensor.h>
|
||||
|
||||
#include <board_config.h>
|
||||
|
|
|
@ -59,7 +59,6 @@
|
|||
#include <drivers/drv_hrt.h>
|
||||
|
||||
#include <uORB/uORB.h>
|
||||
#include <uORB/topics/subsystem_info.h>
|
||||
#include <uORB/topics/distance_sensor.h>
|
||||
|
||||
#include <board_config.h>
|
||||
|
|
Loading…
Reference in New Issue