mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-07-01 23:00:35 +08:00
Merge branch 'master' into rc_timeout
This commit is contained in:
@@ -1,6 +1,6 @@
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/****************************************************************************
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*
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* Copyright (C) 2013 PX4 Development Team. All rights reserved.
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* Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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@@ -64,9 +64,9 @@ int do_airspeed_calibration(int mavlink_fd)
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{
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/* give directions */
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mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name);
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mavlink_log_info(mavlink_fd, "don't move system");
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mavlink_log_info(mavlink_fd, "ensure airspeed sensor is not registering wind");
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const int calibration_count = 2500;
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const int calibration_count = 2000;
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int diff_pres_sub = orb_subscribe(ORB_ID(differential_pressure));
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struct differential_pressure_s diff_pres;
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@@ -85,13 +85,15 @@ int do_airspeed_calibration(int mavlink_fd)
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if (fd > 0) {
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if (OK == ioctl(fd, AIRSPEEDIOCSSCALE, (long unsigned int)&airscale)) {
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paramreset_successful = true;
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} else {
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mavlink_log_critical(mavlink_fd, "airspeed offset zero failed");
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}
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close(fd);
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}
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if (!paramreset_successful) {
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warn("WARNING: failed to set scale / offsets for airspeed sensor");
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mavlink_log_critical(mavlink_fd, "could not reset dpress sensor");
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warn("FAILED to set scale / offsets for airspeed");
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mavlink_log_critical(mavlink_fd, "dpress reset failed");
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mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name);
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return ERROR;
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}
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@@ -107,7 +109,7 @@ int do_airspeed_calibration(int mavlink_fd)
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if (poll_ret) {
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orb_copy(ORB_ID(differential_pressure), diff_pres_sub, &diff_pres);
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diff_pres_offset += diff_pres.differential_pressure_pa;
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diff_pres_offset += diff_pres.differential_pressure_raw_pa;
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calibration_counter++;
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if (calibration_counter % (calibration_count / 20) == 0)
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@@ -1503,7 +1503,7 @@ Navigator::check_mission_item_reached()
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/* check yaw if defined only for rotary wing except takeoff */
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float yaw_err = _wrap_pi(_mission_item.yaw - _global_pos.yaw);
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if (fabsf(yaw_err) < 0.05f) { /* XXX get rid of magic number */
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if (fabsf(yaw_err) < 0.2f) { /* XXX get rid of magic number */
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_waypoint_yaw_reached = true;
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}
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@@ -84,6 +84,8 @@
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#include <uORB/topics/esc_status.h>
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#include <uORB/topics/telemetry_status.h>
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#include <uORB/topics/estimator_status.h>
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#include <uORB/topics/system_power.h>
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#include <uORB/topics/servorail_status.h>
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#include <systemlib/systemlib.h>
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#include <systemlib/param/param.h>
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@@ -796,6 +798,8 @@ int sdlog2_thread_main(int argc, char *argv[])
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struct telemetry_status_s telemetry;
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struct range_finder_report range_finder;
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struct estimator_status_report estimator_status;
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struct system_power_s system_power;
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struct servorail_status_s servorail_status;
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} buf;
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memset(&buf, 0, sizeof(buf));
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@@ -828,6 +832,7 @@ int sdlog2_thread_main(int argc, char *argv[])
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struct log_DIST_s log_DIST;
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struct log_TELE_s log_TELE;
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struct log_ESTM_s log_ESTM;
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struct log_PWR_s log_PWR;
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} body;
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} log_msg = {
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LOG_PACKET_HEADER_INIT(0)
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@@ -859,6 +864,8 @@ int sdlog2_thread_main(int argc, char *argv[])
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int telemetry_sub;
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int range_finder_sub;
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int estimator_status_sub;
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int system_power_sub;
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int servorail_status_sub;
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} subs;
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subs.cmd_sub = orb_subscribe(ORB_ID(vehicle_command));
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@@ -884,6 +891,8 @@ int sdlog2_thread_main(int argc, char *argv[])
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subs.telemetry_sub = orb_subscribe(ORB_ID(telemetry_status));
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subs.range_finder_sub = orb_subscribe(ORB_ID(sensor_range_finder));
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subs.estimator_status_sub = orb_subscribe(ORB_ID(estimator_status));
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subs.system_power_sub = orb_subscribe(ORB_ID(system_power));
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subs.servorail_status_sub = orb_subscribe(ORB_ID(servorail_status));
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thread_running = true;
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@@ -1185,6 +1194,7 @@ int sdlog2_thread_main(int argc, char *argv[])
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log_msg.msg_type = LOG_AIRS_MSG;
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log_msg.body.log_AIRS.indicated_airspeed = buf.airspeed.indicated_airspeed_m_s;
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log_msg.body.log_AIRS.true_airspeed = buf.airspeed.true_airspeed_m_s;
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log_msg.body.log_AIRS.air_temperature_celsius = buf.airspeed.air_temperature_celsius;
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LOGBUFFER_WRITE_AND_COUNT(AIRS);
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}
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@@ -1227,6 +1237,24 @@ int sdlog2_thread_main(int argc, char *argv[])
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LOGBUFFER_WRITE_AND_COUNT(BATT);
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}
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/* --- SYSTEM POWER RAILS --- */
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if (copy_if_updated(ORB_ID(system_power), subs.system_power_sub, &buf.system_power)) {
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log_msg.msg_type = LOG_PWR_MSG;
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log_msg.body.log_PWR.peripherals_5v = buf.system_power.voltage5V_v;
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log_msg.body.log_PWR.usb_ok = buf.system_power.usb_connected;
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log_msg.body.log_PWR.brick_ok = buf.system_power.brick_valid;
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log_msg.body.log_PWR.servo_ok = buf.system_power.servo_valid;
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log_msg.body.log_PWR.low_power_rail_overcurrent = buf.system_power.periph_5V_OC;
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log_msg.body.log_PWR.high_power_rail_overcurrent = buf.system_power.hipower_5V_OC;
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/* copy servo rail status topic here too */
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orb_copy(ORB_ID(servorail_status), subs.servorail_status_sub, &buf.servorail_status);
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log_msg.body.log_PWR.servo_rail_5v = buf.servorail_status.voltage_v;
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log_msg.body.log_PWR.servo_rssi = buf.servorail_status.rssi_v;
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LOGBUFFER_WRITE_AND_COUNT(PWR);
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}
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/* --- TELEMETRY --- */
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if (copy_if_updated(ORB_ID(telemetry_status), subs.telemetry_sub, &buf.telemetry)) {
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log_msg.msg_type = LOG_TELE_MSG;
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@@ -175,6 +175,7 @@ struct log_OUT0_s {
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struct log_AIRS_s {
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float indicated_airspeed;
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float true_airspeed;
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float air_temperature_celsius;
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};
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/* --- ARSP - ATTITUDE RATE SET POINT --- */
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@@ -278,6 +279,29 @@ struct log_TELE_s {
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uint8_t txbuf;
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};
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/* --- ESTM - ESTIMATOR STATUS --- */
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#define LOG_ESTM_MSG 23
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struct log_ESTM_s {
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float s[10];
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uint8_t n_states;
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uint8_t states_nan;
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uint8_t covariance_nan;
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uint8_t kalman_gain_nan;
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};
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/* --- PWR - ONBOARD POWER SYSTEM --- */
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#define LOG_PWR_MSG 24
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struct log_PWR_s {
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float peripherals_5v;
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float servo_rail_5v;
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float servo_rssi;
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uint8_t usb_ok;
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uint8_t brick_ok;
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uint8_t servo_ok;
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uint8_t low_power_rail_overcurrent;
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uint8_t high_power_rail_overcurrent;
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};
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/********** SYSTEM MESSAGES, ID > 0x80 **********/
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/* --- TIME - TIME STAMP --- */
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@@ -300,23 +324,6 @@ struct log_PARM_s {
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float value;
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};
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/* --- ESTM - ESTIMATOR STATUS --- */
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#define LOG_ESTM_MSG 132
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struct log_ESTM_s {
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float s[10];
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uint8_t n_states;
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uint8_t states_nan;
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uint8_t covariance_nan;
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uint8_t kalman_gain_nan;
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};
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// struct log_ESTM_s {
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// float s[32];
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// uint8_t n_states;
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// uint8_t states_nan;
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// uint8_t covariance_nan;
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// uint8_t kalman_gain_nan;
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// };
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#pragma pack(pop)
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/* construct list of all message formats */
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@@ -333,7 +340,7 @@ static const struct log_format_s log_formats[] = {
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LOG_FORMAT(STAT, "BBfBB", "MainState,ArmState,BatRem,BatWarn,Landed"),
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LOG_FORMAT(RC, "ffffffffBB", "Ch0,Ch1,Ch2,Ch3,Ch4,Ch5,Ch6,Ch7,Count,SignalLost"),
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LOG_FORMAT(OUT0, "ffffffff", "Out0,Out1,Out2,Out3,Out4,Out5,Out6,Out7"),
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LOG_FORMAT(AIRS, "ff", "IndSpeed,TrueSpeed"),
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LOG_FORMAT(AIRS, "fff", "IndSpeed,TrueSpeed,AirTemp"),
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LOG_FORMAT(ARSP, "fff", "RollRateSP,PitchRateSP,YawRateSP"),
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LOG_FORMAT(FLOW, "hhfffBB", "RawX,RawY,CompX,CompY,Dist,Q,SensID"),
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LOG_FORMAT(GPOS, "LLfffffB", "Lat,Lon,Alt,VelN,VelE,VelD,BaroAlt,Flags"),
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@@ -343,16 +350,16 @@ static const struct log_format_s log_formats[] = {
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LOG_FORMAT(BATT, "ffff", "V,VFilt,C,Discharged"),
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LOG_FORMAT(DIST, "ffB", "Bottom,BottomRate,Flags"),
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LOG_FORMAT(TELE, "BBBBHHB", "RSSI,RemRSSI,Noise,RemNoise,RXErr,Fixed,TXBuf"),
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LOG_FORMAT(ESTM, "ffffffffffBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,n_states,states_nan,cov_nan,kgain_nan"),
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LOG_FORMAT(PWR, "fffBBBBB", "Periph_5V,Servo_5V,RSSI,USB_OK,BRICK_OK,SRV_OK,PERIPH_OC,HIPWR_OC"),
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/* system-level messages, ID >= 0x80 */
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// FMT: don't write format of format message, it's useless
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/* FMT: don't write format of format message, it's useless */
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LOG_FORMAT(TIME, "Q", "StartTime"),
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LOG_FORMAT(VER, "NZ", "Arch,FwGit"),
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LOG_FORMAT(PARM, "Nf", "Name,Value"),
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LOG_FORMAT(ESTM, "ffffffffffBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,n_states,states_nan,cov_nan,kgain_nan"),
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//LOG_FORMAT(ESTM, "ffffffffffffffffffffffffffffffffBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,s10,s11,s12,s13,s14,s15,s16,s17,s18,s19,s20,s21,s22,s23,s24,s25,s26,s27,s28,s29,s30,s31,n_states,states_nan,cov_nan,kgain_nan"),
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LOG_FORMAT(PARM, "Nf", "Name,Value")
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};
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static const int log_formats_num = sizeof(log_formats) / sizeof(struct log_format_s);
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static const unsigned log_formats_num = sizeof(log_formats) / sizeof(log_formats[0]);
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#endif /* SDLOG2_MESSAGES_H_ */
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@@ -1013,12 +1013,13 @@ Sensors::diff_pres_poll(struct sensor_combined_s &raw)
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raw.differential_pressure_timestamp = _diff_pres.timestamp;
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raw.differential_pressure_filtered_pa = _diff_pres.differential_pressure_filtered_pa;
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float air_temperature_celcius = (_diff_pres.temperature > -300.0f) ? _diff_pres.temperature : (raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG);
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float air_temperature_celsius = (_diff_pres.temperature > -300.0f) ? _diff_pres.temperature : (raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG);
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_airspeed.timestamp = _diff_pres.timestamp;
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_airspeed.indicated_airspeed_m_s = calc_indicated_airspeed(_diff_pres.differential_pressure_filtered_pa);
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_airspeed.true_airspeed_m_s = calc_true_airspeed(_diff_pres.differential_pressure_filtered_pa + raw.baro_pres_mbar * 1e2f,
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raw.baro_pres_mbar * 1e2f, air_temperature_celcius);
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raw.baro_pres_mbar * 1e2f, air_temperature_celsius);
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_airspeed.air_temperature_celsius = air_temperature_celsius;
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/* announce the airspeed if needed, just publish else */
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if (_airspeed_pub > 0) {
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@@ -90,6 +90,9 @@ ORB_DEFINE(battery_status, struct battery_status_s);
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#include "topics/servorail_status.h"
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ORB_DEFINE(servorail_status, struct servorail_status_s);
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#include "topics/system_power.h"
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ORB_DEFINE(system_power, struct system_power_s);
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#include "topics/vehicle_global_position.h"
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ORB_DEFINE(vehicle_global_position, struct vehicle_global_position_s);
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@@ -52,9 +52,10 @@
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* Airspeed
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*/
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struct airspeed_s {
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uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
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uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
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float indicated_airspeed_m_s; /**< indicated airspeed in meters per second, -1 if unknown */
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float true_airspeed_m_s; /**< true airspeed in meters per second, -1 if unknown */
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float true_airspeed_m_s; /**< true airspeed in meters per second, -1 if unknown */
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float air_temperature_celsius; /**< air temperature in degrees celsius, -1000 if unknown */
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};
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/**
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@@ -52,13 +52,14 @@
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* Differential pressure.
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*/
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struct differential_pressure_s {
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uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
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uint64_t error_count;
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uint64_t timestamp; /**< Microseconds since system boot, needed to integrate */
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uint64_t error_count; /**< Number of errors detected by driver */
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float differential_pressure_pa; /**< Differential pressure reading */
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float differential_pressure_raw_pa; /**< Raw differential pressure reading (may be negative) */
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float differential_pressure_filtered_pa; /**< Low pass filtered differential pressure reading */
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float max_differential_pressure_pa; /**< Maximum differential pressure reading */
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float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */
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float temperature; /**< Temperature provided by sensor, -1000.0f if unknown */
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float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */
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float temperature; /**< Temperature provided by sensor, -1000.0f if unknown */
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};
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@@ -0,0 +1,71 @@
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/****************************************************************************
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*
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* Copyright (C) 2012-2013 PX4 Development Team. All rights reserved.
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*
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* 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.
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||||
*
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||||
* 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.
|
||||
*
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||||
****************************************************************************/
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||||
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/**
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* @file system_power.h
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*
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* Definition of the system_power voltage and power status uORB topic.
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||||
*/
|
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#ifndef SYSTEM_POWER_H_
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#define SYSTEM_POWER_H_
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#include "../uORB.h"
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#include <stdint.h>
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/**
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* @addtogroup topics
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||||
* @{
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||||
*/
|
||||
|
||||
/**
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* voltage and power supply status
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*/
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struct system_power_s {
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uint64_t timestamp; /**< microseconds since system boot */
|
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float voltage5V_v; /**< peripheral 5V rail voltage */
|
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uint8_t usb_connected:1; /**< USB is connected when 1 */
|
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uint8_t brick_valid:1; /**< brick power is good when 1 */
|
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uint8_t servo_valid:1; /**< servo power is good when 1 */
|
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uint8_t periph_5V_OC:1; /**< peripheral overcurrent when 1 */
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uint8_t hipower_5V_OC:1; /**< hi power peripheral overcurrent when 1 */
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};
|
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|
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/**
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* @}
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*/
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/* register this as object request broker structure */
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ORB_DECLARE(system_power);
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#endif
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Reference in New Issue
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