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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-03 16:18:52 +08:00
Add the HighLatency2 mavlink stream
This commit is contained in:
@@ -73,6 +73,7 @@
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#include <uORB/topics/distance_sensor.h>
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#include <uORB/topics/estimator_status.h>
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#include <uORB/topics/fw_pos_ctrl_status.h>
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#include <uORB/topics/geofence_result.h>
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#include <uORB/topics/home_position.h>
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#include <uORB/topics/manual_control_setpoint.h>
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#include <uORB/topics/mavlink_log.h>
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@@ -94,6 +95,7 @@
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#include <uORB/topics/vehicle_local_position_setpoint.h>
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#include <uORB/topics/vehicle_rates_setpoint.h>
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#include <uORB/topics/vehicle_status.h>
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#include <uORB/topics/vehicle_status_flags.h>
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#include <uORB/topics/vtol_vehicle_status.h>
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#include <uORB/topics/wind_estimate.h>
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#include <uORB/topics/mount_orientation.h>
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@@ -3931,22 +3933,22 @@ protected:
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}
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};
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class MavlinkStreamHighLatency : public MavlinkStream
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class MavlinkStreamHighLatency2 : public MavlinkStream
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{
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public:
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const char *get_name() const
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{
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return MavlinkStreamHighLatency::get_name_static();
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return MavlinkStreamHighLatency2::get_name_static();
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}
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static const char *get_name_static()
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{
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return "HIGH_LATENCY";
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return "HIGH_LATENCY2";
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}
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static uint16_t get_id_static()
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{
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return MAVLINK_MSG_ID_HIGH_LATENCY;
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return MAVLINK_MSG_ID_HIGH_LATENCY2;
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}
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uint16_t get_id()
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@@ -3956,17 +3958,20 @@ public:
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static MavlinkStream *new_instance(Mavlink *mavlink)
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{
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return new MavlinkStreamHighLatency(mavlink);
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return new MavlinkStreamHighLatency2(mavlink);
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}
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unsigned get_size()
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{
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return MAVLINK_MSG_ID_HIGH_LATENCY_LEN + MAVLINK_NUM_NON_PAYLOAD_BYTES;
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return MAVLINK_MSG_ID_HIGH_LATENCY2_LEN + MAVLINK_NUM_NON_PAYLOAD_BYTES;
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}
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private:
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MavlinkOrbSubscription *_actuator_sub;
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uint64_t _actuator_time;
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MavlinkOrbSubscription *_actuator_sub_0;
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uint64_t _actuator_time_0;
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MavlinkOrbSubscription *_actuator_sub_1;
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uint64_t _actuator_time_1;
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MavlinkOrbSubscription *_airspeed_sub;
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uint64_t _airspeed_time;
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@@ -3974,168 +3979,503 @@ private:
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MavlinkOrbSubscription *_attitude_sp_sub;
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uint64_t _attitude_sp_time;
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MavlinkOrbSubscription *_attitude_sub;
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uint64_t _attitude_time;
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MavlinkOrbSubscription *_battery_sub;
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uint64_t _battery_time;
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MavlinkOrbSubscription *_estimator_status_sub;
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uint64_t _estimator_status_time;
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MavlinkOrbSubscription *_fw_pos_ctrl_status_sub;
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uint64_t _fw_pos_ctrl_status_time;
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MavlinkOrbSubscription *_geofence_sub;
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uint64_t _geofence_time;
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MavlinkOrbSubscription *_global_pos_sub;
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uint64_t _global_pos_time;
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MavlinkOrbSubscription *_gps_sub;
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uint64_t _gps_time;
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MavlinkOrbSubscription *_home_sub;
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uint64_t _home_time;
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MavlinkOrbSubscription *_landed_sub;
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uint64_t _landed_time;
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MavlinkOrbSubscription *_mission_result_sub;
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uint64_t _mission_result_time;
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MavlinkOrbSubscription *_sensor_sub;
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uint64_t _sensor_time;
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MavlinkOrbSubscription *_status_sub;
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uint64_t _status_time;
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MavlinkOrbSubscription *_status_flags_sub;
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uint64_t _status_flags_time;
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MavlinkOrbSubscription *_tecs_status_sub;
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uint64_t _tecs_time;
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MavlinkOrbSubscription *_wind_sub;
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uint64_t _wind_time;
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SimpleAnalyzer _airspeed;
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SimpleAnalyzer _airspeed_sp;
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SimpleAnalyzer _battery;
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SimpleAnalyzer _climb_rate;
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SimpleAnalyzer _eph;
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SimpleAnalyzer _epv;
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SimpleAnalyzer _groundspeed;
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SimpleAnalyzer _temperature;
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SimpleAnalyzer _throttle;
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SimpleAnalyzer _windspeed;
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/* do not allow top copying this class */
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MavlinkStreamHighLatency(MavlinkStreamHighLatency &);
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MavlinkStreamHighLatency &operator = (const MavlinkStreamHighLatency &);
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MavlinkStreamHighLatency2(MavlinkStreamHighLatency2 &);
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MavlinkStreamHighLatency2 &operator = (const MavlinkStreamHighLatency2 &);
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protected:
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explicit MavlinkStreamHighLatency(Mavlink *mavlink) : MavlinkStream(mavlink),
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_actuator_sub(_mavlink->add_orb_subscription(ORB_ID(actuator_controls_0))),
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_actuator_time(0),
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explicit MavlinkStreamHighLatency2(Mavlink *mavlink) : MavlinkStream(mavlink),
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_actuator_sub_0(_mavlink->add_orb_subscription(ORB_ID(actuator_controls_0))),
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_actuator_time_0(0),
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_actuator_sub_1(_mavlink->add_orb_subscription(ORB_ID(actuator_controls_1))),
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_actuator_time_1(0),
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_airspeed_sub(_mavlink->add_orb_subscription(ORB_ID(airspeed))),
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_airspeed_time(0),
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_attitude_sp_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_attitude_setpoint))),
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_attitude_sp_time(0),
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_attitude_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_attitude))),
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_attitude_time(0),
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_battery_sub(_mavlink->add_orb_subscription(ORB_ID(battery_status))),
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_battery_time(0),
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_estimator_status_sub(_mavlink->add_orb_subscription(ORB_ID(estimator_status))),
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_estimator_status_time(0),
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_fw_pos_ctrl_status_sub(_mavlink->add_orb_subscription(ORB_ID(fw_pos_ctrl_status))),
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_fw_pos_ctrl_status_time(0),
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_geofence_sub(_mavlink->add_orb_subscription(ORB_ID(geofence_result))),
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_geofence_time(0),
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_global_pos_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_global_position))),
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_global_pos_time(0),
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_gps_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_gps_position))),
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_gps_time(0),
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_home_sub(_mavlink->add_orb_subscription(ORB_ID(home_position))),
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_home_time(0),
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_landed_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_land_detected))),
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_landed_time(0),
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_mission_result_sub(_mavlink->add_orb_subscription(ORB_ID(mission_result))),
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_mission_result_time(0),
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_sensor_sub(_mavlink->add_orb_subscription(ORB_ID(sensor_combined))),
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_sensor_time(0),
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_status_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_status))),
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_status_time(0),
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_status_flags_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_status_flags))),
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_status_flags_time(0),
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_tecs_status_sub(_mavlink->add_orb_subscription(ORB_ID(tecs_status))),
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_tecs_time(0)
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_tecs_time(0),
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_wind_sub(_mavlink->add_orb_subscription(ORB_ID(wind_estimate))),
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_wind_time(0),
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_airspeed(SimpleAnalyzer::AVERAGE),
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_airspeed_sp(SimpleAnalyzer::AVERAGE),
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_battery(SimpleAnalyzer::AVERAGE),
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_climb_rate(SimpleAnalyzer::MAX),
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_eph(SimpleAnalyzer::MAX),
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_epv(SimpleAnalyzer::MAX),
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_groundspeed(SimpleAnalyzer::AVERAGE),
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_temperature(SimpleAnalyzer::AVERAGE),
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_throttle(SimpleAnalyzer::AVERAGE),
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_windspeed(SimpleAnalyzer::AVERAGE)
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{}
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bool send(const hrt_abstime t)
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{
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actuator_controls_s actuator = {};
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airspeed_s airspeed = {};
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battery_status_s battery = {};
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fw_pos_ctrl_status_s fw_pos_ctrl_status = {};
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home_position_s home = {};
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mission_result_s mission_result = {};
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sensor_combined_s sensor = {};
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tecs_status_s tecs_status = {};
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vehicle_attitude_s attitude = {};
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vehicle_attitude_setpoint_s attitude_sp = {};
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vehicle_global_position_s global_pos = {};
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vehicle_gps_position_s gps = {};
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vehicle_land_detected_s land_detected = {};
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vehicle_status_s status = {};
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struct airspeed_s airspeed = {};
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struct battery_status_s battery = {};
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struct estimator_status_s estimator_status = {};
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struct fw_pos_ctrl_status_s fw_pos_ctrl_status = {};
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struct mission_result_s mission_result = {};
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struct geofence_result_s geofence = {};
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struct tecs_status_s tecs_status = {};
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struct vehicle_attitude_setpoint_s attitude_sp = {};
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struct vehicle_global_position_s global_pos = {};
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struct vehicle_status_s status = {};
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struct vehicle_status_flags_s status_flags = {};
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struct wind_estimate_s wind = {};
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bool updated = _status_sub->update(&_status_time, &status);
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updated |= _actuator_sub->update(&_actuator_time, &actuator);
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updated |= _airspeed_sub->update(&_airspeed_time, &airspeed);
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bool updated = _airspeed_sub->update(&_airspeed_time, &airspeed);
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updated |= _airspeed.valid();
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updated |= _airspeed_sp.valid();
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updated |= _battery.valid();
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updated |= _climb_rate.valid();
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updated |= _eph.valid();
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updated |= _epv.valid();
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updated |= _groundspeed.valid();
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updated |= _temperature.valid();
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updated |= _throttle.valid();
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updated |= _windspeed.valid();
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updated |= _attitude_sp_sub->update(&_attitude_sp_time, &attitude_sp);
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updated |= _attitude_sub->update(&_attitude_time, &attitude);
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updated |= _battery_sub->update(&_battery_time, &battery);
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updated |= _estimator_status_sub->update(&_estimator_status_time, &estimator_status);
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updated |= _fw_pos_ctrl_status_sub->update(&_fw_pos_ctrl_status_time, &fw_pos_ctrl_status);
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updated |= _geofence_sub->update(&_geofence_time, &geofence);
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updated |= _global_pos_sub->update(&_global_pos_time, &global_pos);
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updated |= _gps_sub->update(&_gps_time, &gps);
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updated |= _home_sub->update(&_home_time, &home);
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updated |= _landed_sub->update(&_landed_time, &land_detected);
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updated |= _mission_result_sub->update(&_mission_result_time, &mission_result);
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updated |= _sensor_sub->update(&_sensor_time, &sensor);
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updated |= _status_sub->update(&_status_time, &status);
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updated |= _status_flags_sub->update(&_status_flags_time, &status_flags);
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updated |= _tecs_status_sub->update(&_tecs_time, &tecs_status);
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updated |= _wind_sub->update(&_wind_time, &wind);
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if (updated) {
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mavlink_high_latency_t msg = {};
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mavlink_high_latency2_t msg = {};
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set_default_values(msg);
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//timespec tv;
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//px4_clock_gettime(CLOCK_REALTIME, &tv);
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//msg.time_usec = (uint64_t)tv.tv_sec * 1000000 + tv.tv_nsec / 1000;
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convert_limit_safe(t / 1000, &msg.timestamp);
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msg.type = _mavlink->get_system_type();
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msg.autopilot = MAV_AUTOPILOT_PX4;
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msg.base_mode = 0;
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msg.custom_mode = 0;
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uint8_t sys_status;
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get_mavlink_mode_state(&status, &sys_status, &msg.base_mode, &msg.custom_mode);
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matrix::Eulerf euler = matrix::Quatf(attitude.q);
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msg.roll = math::degrees(euler.phi()) * 100;
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msg.pitch = math::degrees(euler.theta()) * 100;
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msg.heading = math::degrees(_wrap_2pi(euler.psi())) * 100;
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//msg.roll_sp = math::degrees(attitude_sp.roll_body) * 100;
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//msg.pitch_sp = math::degrees(attitude_sp.pitch_body) * 100;
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msg.heading_sp = math::degrees(_wrap_2pi(attitude_sp.yaw_body)) * 100;
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if (status.arming_state == vehicle_status_s::ARMING_STATE_ARMED) {
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msg.throttle = actuator.control[actuator_controls_s::INDEX_THROTTLE] * 100;
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} else {
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msg.throttle = 0;
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if (_attitude_sp_time > 0) {
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msg.target_heading = static_cast<uint8_t>(math::degrees(_wrap_2pi(attitude_sp.yaw_body)) * 0.5f);
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}
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msg.latitude = global_pos.lat * 1e7;
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msg.longitude = global_pos.lon * 1e7;
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if (_fw_pos_ctrl_status_time > 0) {
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convert_limit_safe(fw_pos_ctrl_status.wp_dist * 0.1f, &msg.target_distance);
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}
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//msg.altitude_home = (_home_time > 0) ? (global_pos.alt - home.alt) : NAN;
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msg.altitude_amsl = (_global_pos_time > 0) ? global_pos.alt : NAN;
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if (_global_pos_time > 0) {
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convert_limit_safe(global_pos.lat * 1e7, &msg.latitude);
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convert_limit_safe(global_pos.lon * 1e7, &msg.longitude);
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msg.altitude_sp = ((_tecs_time > 0) && home.valid_alt) ? (tecs_status.altitudeSp - home.alt) : NAN;
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if (global_pos.alt > 0) {
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convert_limit_safe(global_pos.alt + 0.5f, &msg.altitude);
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msg.airspeed = airspeed.indicated_airspeed_m_s * 100.0f;
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msg.groundspeed = sqrtf(global_pos.vel_n * global_pos.vel_n + global_pos.vel_e * global_pos.vel_e) * 100.0f;
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msg.climb_rate = -global_pos.vel_d;
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} else {
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convert_limit_safe(global_pos.alt - 0.5f, &msg.altitude);
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}
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msg.gps_nsat = gps.satellites_used;
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msg.gps_fix_type = gps.fix_type;
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msg.heading = static_cast<uint8_t>(math::degrees(_wrap_2pi(global_pos.yaw)) * 0.5f);
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}
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msg.landed_state = land_detected.landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR;
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if (_mission_result_time > 0) {
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msg.wp_num = mission_result.seq_current;
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}
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msg.battery_remaining = (battery.connected) ? battery.remaining * 100.0f : -1;
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if (_tecs_time > 0) {
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convert_limit_safe(tecs_status.altitudeSp, &msg.target_altitude);
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}
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msg.temperature = sensor.baro_temp_celcius;
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msg.temperature_air = airspeed.air_temperature_celsius;
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if (_wind_time > 0) {
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msg.wind_heading = static_cast<uint8_t>(
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math::degrees(_wrap_2pi(atan2f(wind.windspeed_east, wind.windspeed_north))) * 0.5f);
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}
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msg.wp_num = mission_result.seq_current;
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msg.wp_distance = fw_pos_ctrl_status.wp_dist;
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if (_airspeed.valid()) {
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_airspeed.get_scaled(msg.airspeed, 5.0f);
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}
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mavlink_msg_high_latency_send_struct(_mavlink->get_channel(), &msg);
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if (_airspeed_sp.valid()) {
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_airspeed_sp.get_scaled(msg.airspeed_sp, 5.0f);
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}
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if (_battery.valid()) {
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_battery.get_scaled(msg.battery, 100.0f);
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}
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if (_climb_rate.valid()) {
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_climb_rate.get_scaled(msg.climb_rate, 10.0f);
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}
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if (_eph.valid()) {
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_eph.get_scaled(msg.eph, 10.0f);
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}
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if (_epv.valid()) {
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_epv.get_scaled(msg.epv, 10.0f);
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}
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if (_groundspeed.valid()) {
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_groundspeed.get_scaled(msg.groundspeed, 5.0f);
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}
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if (_temperature.valid()) {
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_temperature.get_scaled(msg.temperature_air, 1.0f);
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}
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if (_throttle.valid()) {
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_throttle.get_scaled(msg.throttle, 100.0f);
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}
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if (_windspeed.valid()) {
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_windspeed.get_scaled(msg.windspeed, 5.0f);
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}
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// failsafe flags, requires an initial value of 0
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if (_battery_time > 0) {
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if (battery.warning > battery_status_s::BATTERY_WARNING_LOW) {
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msg.failsafe |= MAV_FAILSAFE_FLAG_BATTERY;
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}
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}
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if (_status_time > 0) {
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if (status.rc_signal_lost) {
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msg.failsafe |= MAV_FAILSAFE_FLAG_RC_LOSS;
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}
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if (status.engine_failure) {
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msg.failsafe |= MAV_FAILSAFE_FLAG_ENGINE;
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}
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if (status.data_link_lost) {
|
||||
msg.failsafe |= MAV_FAILSAFE_FLAG_TELEM_LOSS;
|
||||
}
|
||||
}
|
||||
|
||||
if (_geofence_time > 0) {
|
||||
if (geofence.geofence_violated) {
|
||||
msg.failsafe |= MAV_FAILSAFE_FLAG_GEOFENCE;
|
||||
}
|
||||
}
|
||||
|
||||
if (_status_flags_time > 0) {
|
||||
if (status_flags.gps_failure || !status_flags.condition_global_position_valid) {
|
||||
msg.failsafe |= MAV_FAILSAFE_FLAG_GPS;
|
||||
}
|
||||
}
|
||||
|
||||
// failure flags
|
||||
|
||||
if (_airspeed_time > 0) {
|
||||
if (airspeed.confidence < 0.95f) { // the same threshold as for the commander
|
||||
msg.failure_flags |= MAV_FAILURE_FLAG_AIRSPEED;
|
||||
}
|
||||
}
|
||||
|
||||
if (_estimator_status_time > 0) {
|
||||
if (estimator_status.gps_check_fail_flags > 0 ||
|
||||
estimator_status.filter_fault_flags > 0 ||
|
||||
estimator_status.innovation_check_flags > 0) {
|
||||
msg.failure_flags |= MAV_FAILURE_FLAG_ESTIMATOR;
|
||||
}
|
||||
}
|
||||
|
||||
if (_status_flags_time > 0) {
|
||||
if (status_flags.gps_failure) {
|
||||
msg.failure_flags |= MAV_FAILURE_FLAG_GPS;
|
||||
}
|
||||
|
||||
if (status_flags.offboard_control_signal_lost && status_flags.offboard_control_signal_found_once) {
|
||||
msg.failure_flags |= MAV_FAILURE_FLAG_OFFBOARD_LINK;
|
||||
}
|
||||
}
|
||||
|
||||
if (_status_time > 0) {
|
||||
if (((status.onboard_control_sensors_enabled & MAV_SYS_STATUS_SENSOR_3D_ACCEL)
|
||||
&& !(status.onboard_control_sensors_health & MAV_SYS_STATUS_SENSOR_3D_ACCEL)) ||
|
||||
((status.onboard_control_sensors_enabled & MAV_SYS_STATUS_SENSOR_3D_ACCEL2) &&
|
||||
!(status.onboard_control_sensors_health & MAV_SYS_STATUS_SENSOR_3D_ACCEL2))) {
|
||||
msg.failure_flags |= MAV_FAILURE_FLAG_ACCELEROMETER;
|
||||
}
|
||||
|
||||
if ((status.onboard_control_sensors_enabled & MAV_SYS_STATUS_SENSOR_ABSOLUTE_PRESSURE)
|
||||
&& !(status.onboard_control_sensors_health & MAV_SYS_STATUS_SENSOR_ABSOLUTE_PRESSURE)) {
|
||||
msg.failure_flags |= MAV_FAILURE_FLAG_BAROMETER;
|
||||
}
|
||||
|
||||
if (((status.onboard_control_sensors_enabled & MAV_SYS_STATUS_SENSOR_3D_GYRO)
|
||||
&& !(status.onboard_control_sensors_health & MAV_SYS_STATUS_SENSOR_3D_GYRO)) ||
|
||||
((status.onboard_control_sensors_enabled & MAV_SYS_STATUS_SENSOR_3D_GYRO2) &&
|
||||
!(status.onboard_control_sensors_health & MAV_SYS_STATUS_SENSOR_3D_GYRO2))) {
|
||||
msg.failure_flags |= MAV_FAILURE_FLAG_GYROSCOPE;
|
||||
}
|
||||
|
||||
if ((status.onboard_control_sensors_enabled & MAV_SYS_STATUS_SENSOR_LASER_POSITION)
|
||||
&& !(status.onboard_control_sensors_health & MAV_SYS_STATUS_SENSOR_LASER_POSITION)) {
|
||||
msg.failure_flags |= MAV_FAILURE_FLAG_LIDAR;
|
||||
}
|
||||
|
||||
if (((status.onboard_control_sensors_enabled & MAV_SYS_STATUS_SENSOR_3D_MAG)
|
||||
&& !(status.onboard_control_sensors_health & MAV_SYS_STATUS_SENSOR_3D_MAG)) ||
|
||||
((status.onboard_control_sensors_enabled & MAV_SYS_STATUS_SENSOR_3D_MAG2) &&
|
||||
!(status.onboard_control_sensors_health & MAV_SYS_STATUS_SENSOR_3D_MAG2))) {
|
||||
msg.failure_flags |= MAV_FAILURE_FLAG_MAGNETOMETER;
|
||||
}
|
||||
|
||||
if (status.mission_failure) {
|
||||
msg.failure_flags |= MAV_FAILURE_FLAG_MISSION;
|
||||
}
|
||||
}
|
||||
|
||||
// flight mode
|
||||
switch (status.nav_state) {
|
||||
case vehicle_status_s::NAVIGATION_STATE_MANUAL:
|
||||
msg.flight_mode = FLIGHT_MODE_MANUAL;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_ALTCTL:
|
||||
msg.flight_mode = FLIGHT_MODE_ALTCTL;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_POSCTL:
|
||||
msg.flight_mode = FLIGHT_MODE_POSCTL;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_AUTO_MISSION:
|
||||
msg.flight_mode = FLIGHT_MODE_AUTO_MISSION;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_AUTO_LOITER:
|
||||
msg.flight_mode = FLIGHT_MODE_AUTO_LOITER;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_AUTO_RTL:
|
||||
msg.flight_mode = FLIGHT_MODE_AUTO_RTL;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_ACRO:
|
||||
msg.flight_mode = FLIGHT_MODE_ACRO;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_DESCEND:
|
||||
msg.flight_mode = FLIGHT_MODE_DESCEND;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_TERMINATION:
|
||||
msg.flight_mode = FLIGHT_MODE_TERMINATION;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_OFFBOARD:
|
||||
msg.flight_mode = FLIGHT_MODE_OFFBOARD;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_STAB:
|
||||
msg.flight_mode = FLIGHT_MODE_STABILIZED;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_RATTITUDE:
|
||||
msg.flight_mode = FLIGHT_MODE_RATTITIDE;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_AUTO_TAKEOFF:
|
||||
msg.flight_mode = FLIGHT_MODE_AUTO_TAKEOFF;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_AUTO_LAND:
|
||||
msg.flight_mode = FLIGHT_MODE_AUTO_LAND;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_AUTO_FOLLOW_TARGET:
|
||||
msg.flight_mode = FLIGHT_MODE_AUTO_FOLLOW_TARGET;
|
||||
break;
|
||||
|
||||
case vehicle_status_s::NAVIGATION_STATE_AUTO_PRECLAND:
|
||||
msg.flight_mode = FLIGHT_MODE_AUTO_PRECLAND;
|
||||
break;
|
||||
|
||||
default:
|
||||
msg.flight_mode = FLIGHT_MODE_ENUM_END;
|
||||
}
|
||||
|
||||
|
||||
|
||||
// reset the analyzers
|
||||
_airspeed.reset();
|
||||
_airspeed_sp.reset();
|
||||
_battery.reset();
|
||||
_climb_rate.reset();
|
||||
_eph.reset();
|
||||
_epv.reset();
|
||||
_groundspeed.reset();
|
||||
_temperature.reset();
|
||||
_throttle.reset();
|
||||
_windspeed.reset();
|
||||
|
||||
mavlink_msg_high_latency2_send_struct(_mavlink->get_channel(), &msg);
|
||||
}
|
||||
|
||||
return updated;
|
||||
}
|
||||
|
||||
void update_data()
|
||||
{
|
||||
const float update_rate = 1.0f / (_mavlink->get_main_loop_delay() * 1e-6f);
|
||||
|
||||
struct airspeed_s airspeed = {};
|
||||
|
||||
if (_airspeed_sub->update(&airspeed)) {
|
||||
_airspeed.add_value(airspeed.indicated_airspeed_m_s, update_rate);
|
||||
_temperature.add_value(airspeed.air_temperature_celsius, update_rate);
|
||||
}
|
||||
|
||||
struct tecs_status_s tecs_status = {};
|
||||
|
||||
if (_tecs_status_sub->update(&tecs_status)) {
|
||||
_airspeed_sp.add_value(tecs_status.airspeedSp, update_rate);
|
||||
}
|
||||
|
||||
struct battery_status_s battery = {};
|
||||
|
||||
if (_battery_sub->update(&battery)) {
|
||||
_battery.add_value(battery.remaining, update_rate);
|
||||
}
|
||||
|
||||
struct vehicle_global_position_s global_pos = {};
|
||||
|
||||
if (_global_pos_sub->update(&global_pos)) {
|
||||
_climb_rate.add_value(fabs(global_pos.vel_d), update_rate);
|
||||
_groundspeed.add_value(sqrtf(global_pos.vel_n * global_pos.vel_n + global_pos.vel_e * global_pos.vel_e), update_rate);
|
||||
}
|
||||
|
||||
struct vehicle_gps_position_s gps = {};
|
||||
|
||||
if (_gps_sub->update(&gps)) {
|
||||
_eph.add_value(gps.eph, update_rate);
|
||||
_epv.add_value(gps.epv, update_rate);
|
||||
}
|
||||
|
||||
struct vehicle_status_s status = {};
|
||||
|
||||
if (_status_sub->update(&status)) {
|
||||
if (status.arming_state == vehicle_status_s::ARMING_STATE_ARMED) {
|
||||
struct actuator_controls_s actuator = {};
|
||||
|
||||
if (status.is_vtol && !status.is_rotary_wing) {
|
||||
if (_actuator_sub_1->update(&actuator)) {
|
||||
_throttle.add_value(actuator.control[actuator_controls_s::INDEX_THROTTLE], update_rate);
|
||||
}
|
||||
|
||||
} else {
|
||||
if (_actuator_sub_0->update(&actuator)) {
|
||||
_throttle.add_value(actuator.control[actuator_controls_s::INDEX_THROTTLE], update_rate);
|
||||
}
|
||||
}
|
||||
|
||||
} else {
|
||||
_throttle.add_value(0.0f, update_rate);
|
||||
}
|
||||
}
|
||||
|
||||
struct wind_estimate_s wind = {};
|
||||
|
||||
if (_wind_sub->update(&wind)) {
|
||||
_windspeed.add_value(sqrtf(wind.windspeed_north * wind.windspeed_north + wind.windspeed_east * wind.windspeed_east),
|
||||
update_rate);
|
||||
}
|
||||
}
|
||||
|
||||
void set_default_values(mavlink_high_latency2_t &msg) const
|
||||
{
|
||||
msg.airspeed = 0;
|
||||
msg.airspeed_sp = 0;
|
||||
msg.altitude = 0;
|
||||
msg.autopilot = MAV_AUTOPILOT_ENUM_END;
|
||||
msg.battery = -1;
|
||||
msg.climb_rate = 0;
|
||||
msg.custom0 = INT8_MIN;
|
||||
msg.custom1 = INT8_MIN;
|
||||
msg.custom2 = INT8_MIN;
|
||||
msg.eph = UINT8_MAX;
|
||||
msg.epv = UINT8_MAX;
|
||||
msg.failsafe = 0;
|
||||
msg.failure_flags = 0;
|
||||
msg.flight_mode = FLIGHT_MODE_ENUM_END;
|
||||
msg.groundspeed = 0;
|
||||
msg.heading = 0;
|
||||
msg.latitude = 0;
|
||||
msg.longitude = 0;
|
||||
msg.target_altitude = 0;
|
||||
msg.target_distance = 0;
|
||||
msg.target_heading = 0;
|
||||
msg.temperature_air = INT8_MIN;
|
||||
msg.throttle = 0;
|
||||
msg.timestamp = 0;
|
||||
msg.type = MAV_TYPE_ENUM_END;
|
||||
msg.wind_heading = 0;
|
||||
msg.windspeed = 0;
|
||||
msg.wp_num = UINT16_MAX;
|
||||
}
|
||||
};
|
||||
|
||||
|
||||
@@ -4283,7 +4623,7 @@ static const StreamListItem streams_list[] = {
|
||||
StreamListItem(&MavlinkStreamCollision::new_instance, &MavlinkStreamCollision::get_name_static, &MavlinkStreamCollision::get_id_static),
|
||||
StreamListItem(&MavlinkStreamWind::new_instance, &MavlinkStreamWind::get_name_static, &MavlinkStreamWind::get_id_static),
|
||||
StreamListItem(&MavlinkStreamMountOrientation::new_instance, &MavlinkStreamMountOrientation::get_name_static, &MavlinkStreamMountOrientation::get_id_static),
|
||||
StreamListItem(&MavlinkStreamHighLatency::new_instance, &MavlinkStreamHighLatency::get_name_static, &MavlinkStreamHighLatency::get_id_static),
|
||||
StreamListItem(&MavlinkStreamHighLatency2::new_instance, &MavlinkStreamHighLatency2::get_name_static, &MavlinkStreamHighLatency2::get_id_static),
|
||||
StreamListItem(&MavlinkStreamGroundTruth::new_instance, &MavlinkStreamGroundTruth::get_name_static, &MavlinkStreamGroundTruth::get_id_static)
|
||||
};
|
||||
|
||||
@@ -4313,8 +4653,8 @@ MavlinkStream *create_mavlink_stream(const char *stream_name, Mavlink *mavlink)
|
||||
return nullptr;
|
||||
}
|
||||
|
||||
SimpleAnalyzer::SimpleAnalyzer(Mode mode, unsigned int n_max) :
|
||||
_n_max(n_max),
|
||||
SimpleAnalyzer::SimpleAnalyzer(Mode mode, float window) :
|
||||
_window(window),
|
||||
_mode(mode)
|
||||
{
|
||||
reset();
|
||||
@@ -4343,12 +4683,13 @@ void SimpleAnalyzer::reset()
|
||||
_result = FLT_MIN;
|
||||
|
||||
break;
|
||||
|
||||
default:
|
||||
PX4_ERR("SimpleAnalyzer: Unknown mode.");
|
||||
}
|
||||
}
|
||||
|
||||
void SimpleAnalyzer::add_value(float val)
|
||||
void SimpleAnalyzer::add_value(float val, float update_rate)
|
||||
{
|
||||
switch (_mode) {
|
||||
case AVERAGE:
|
||||
@@ -4373,7 +4714,7 @@ void SimpleAnalyzer::add_value(float val)
|
||||
|
||||
// if we get more measurements than n_max so the exponential moving average
|
||||
// is computed
|
||||
if (_n < _n_max) {
|
||||
if ((_n < update_rate * _window) && (update_rate > 1.0f)) {
|
||||
_n++;
|
||||
}
|
||||
|
||||
@@ -4384,22 +4725,22 @@ void SimpleAnalyzer::add_value(float val)
|
||||
}
|
||||
}
|
||||
|
||||
bool SimpleAnalyzer::valid()
|
||||
bool SimpleAnalyzer::valid() const
|
||||
{
|
||||
return _n > 0u;
|
||||
}
|
||||
|
||||
float SimpleAnalyzer::get()
|
||||
float SimpleAnalyzer::get() const
|
||||
{
|
||||
return _result;
|
||||
}
|
||||
|
||||
float SimpleAnalyzer::get_scaled(float scalingfactor)
|
||||
float SimpleAnalyzer::get_scaled(float scalingfactor) const
|
||||
{
|
||||
return get() * scalingfactor;
|
||||
}
|
||||
|
||||
void SimpleAnalyzer::check_limits(float &x, float min, float max)
|
||||
void SimpleAnalyzer::check_limits(float &x, float min, float max) const
|
||||
{
|
||||
if (x > max) {
|
||||
x = max;
|
||||
@@ -4409,7 +4750,7 @@ void SimpleAnalyzer::check_limits(float &x, float min, float max)
|
||||
}
|
||||
}
|
||||
|
||||
void SimpleAnalyzer::int_round(float &x)
|
||||
void SimpleAnalyzer::int_round(float &x) const
|
||||
{
|
||||
if (x < 0) {
|
||||
x -= 0.5f;
|
||||
|
||||
@@ -72,17 +72,17 @@ public:
|
||||
MAX,
|
||||
};
|
||||
|
||||
SimpleAnalyzer(Mode mode, unsigned int n_max = 1000);
|
||||
SimpleAnalyzer(Mode mode, float window = 60.0f);
|
||||
virtual ~SimpleAnalyzer();
|
||||
|
||||
void reset();
|
||||
void add_value(float val);
|
||||
bool valid();
|
||||
float get();
|
||||
float get_scaled(float scalingfactor);
|
||||
void add_value(float val, float update_rate);
|
||||
bool valid() const;
|
||||
float get() const;
|
||||
float get_scaled(float scalingfactor) const;
|
||||
|
||||
template <typename T>
|
||||
void get_scaled(T &ret, float scalingfactor)
|
||||
void get_scaled(T &ret, float scalingfactor) const
|
||||
{
|
||||
float avg = get_scaled(scalingfactor);
|
||||
int_round(avg);
|
||||
@@ -93,12 +93,26 @@ public:
|
||||
|
||||
private:
|
||||
unsigned int _n = 0;
|
||||
unsigned int _n_max = 1000;
|
||||
float _window = 60.0f;
|
||||
Mode _mode = AVERAGE;
|
||||
float _result = 0.0f;
|
||||
|
||||
void check_limits(float &x, float min, float max);
|
||||
void int_round(float &x);
|
||||
void check_limits(float &x, float min, float max) const;
|
||||
void int_round(float &x) const;
|
||||
};
|
||||
|
||||
template<typename Tin, typename Tout>
|
||||
void convert_limit_safe(Tin in, Tout *out)
|
||||
{
|
||||
if (in > std::numeric_limits<Tout>::max()) {
|
||||
*out = std::numeric_limits<Tout>::max();
|
||||
|
||||
} else if (in < std::numeric_limits<Tout>::min()) {
|
||||
*out = std::numeric_limits<Tout>::min();
|
||||
|
||||
} else {
|
||||
*out = static_cast<Tout>(in);
|
||||
}
|
||||
}
|
||||
|
||||
#endif /* MAVLINK_MESSAGES_H_ */
|
||||
|
||||
@@ -71,6 +71,8 @@ MavlinkStream::set_interval(const int interval)
|
||||
int
|
||||
MavlinkStream::update(const hrt_abstime t)
|
||||
{
|
||||
update_data();
|
||||
|
||||
// If the message has never been sent before we want
|
||||
// to send it immediately and can return right away
|
||||
if (_last_sent == 0) {
|
||||
|
||||
@@ -103,6 +103,11 @@ protected:
|
||||
virtual bool send(const hrt_abstime t) = 0;
|
||||
#endif
|
||||
|
||||
/**
|
||||
* Function to collect/update data for the streams when update() is called.
|
||||
*/
|
||||
virtual void update_data() { }
|
||||
|
||||
private:
|
||||
hrt_abstime _last_sent;
|
||||
|
||||
|
||||
Reference in New Issue
Block a user