mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-07-01 02:10:34 +08:00
Merge branch 'master' into paul_estimator_numeric
This commit is contained in:
@@ -1,8 +1,10 @@
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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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* Author: Lorenz Meier
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* Jean Cyr
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* Author: Jean Cyr
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* Lorenz Meier
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* Julian Oes
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* Thomas Gubler
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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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@@ -40,16 +42,8 @@
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#include <nuttx/config.h>
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#include <stdio.h>
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#include <stdlib.h>
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#include <string.h>
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#include <unistd.h>
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#include <fcntl.h>
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#include <errno.h>
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#include <math.h>
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#include <poll.h>
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#include <time.h>
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#include <sys/ioctl.h>
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#include <systemlib/systemlib.h>
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#include <systemlib/err.h>
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#include <queue.h>
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#include "dataman.h"
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@@ -175,8 +169,10 @@ create_work_item(void)
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/* Try to reuse item from free item queue */
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lock_queue(&g_free_q);
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if ((item = (work_q_item_t *)sq_remfirst(&(g_free_q.q))))
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g_free_q.size--;
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unlock_queue(&g_free_q);
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/* If we there weren't any free items then obtain memory for a new one */
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@@ -289,11 +285,11 @@ _write(dm_item_t item, unsigned char index, dm_persitence_t persistence, const v
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offset = calculate_offset(item, index);
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/* If item type or index out of range, return error */
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if (offset < 0)
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if (offset < 0)
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return -1;
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/* Make sure caller has not given us more data than we can handle */
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if (count > DM_MAX_DATA_SIZE)
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if (count > DM_MAX_DATA_SIZE)
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return -1;
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/* Write out the data, prefixed with length and persistence level */
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@@ -339,6 +335,7 @@ _read(dm_item_t item, unsigned char index, void *buf, size_t count)
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/* Read the prefix and data */
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len = -1;
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if (lseek(g_task_fd, offset, SEEK_SET) == offset)
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len = read(g_task_fd, buffer, count + DM_SECTOR_HDR_SIZE);
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@@ -492,7 +489,7 @@ dm_write(dm_item_t item, unsigned char index, dm_persitence_t persistence, const
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return -1;
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/* get a work item and queue up a write request */
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if ((work = create_work_item()) == NULL)
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if ((work = create_work_item()) == NULL)
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return -1;
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work->func = dm_write_func;
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@@ -599,17 +596,20 @@ task_main(int argc, char *argv[])
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/* Open or create the data manager file */
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g_task_fd = open(k_data_manager_device_path, O_RDWR | O_CREAT | O_BINARY);
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if (g_task_fd < 0) {
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warnx("Could not open data manager file %s", k_data_manager_device_path);
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sem_post(&g_init_sema); /* Don't want to hang startup */
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return -1;
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}
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if (lseek(g_task_fd, max_offset, SEEK_SET) != max_offset) {
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close(g_task_fd);
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warnx("Could not seek data manager file %s", k_data_manager_device_path);
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sem_post(&g_init_sema); /* Don't want to hang startup */
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return -1;
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}
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fsync(g_task_fd);
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/* We use two file descriptors, one for the caller context and one for the worker thread */
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@@ -767,10 +767,10 @@ dataman_main(int argc, char *argv[])
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stop();
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else if (!strcmp(argv[1], "status"))
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status();
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else if (!strcmp(argv[1], "poweronrestart"))
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dm_restart(DM_INIT_REASON_POWER_ON);
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else if (!strcmp(argv[1], "inflightrestart"))
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dm_restart(DM_INIT_REASON_IN_FLIGHT);
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else if (!strcmp(argv[1], "poweronrestart"))
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dm_restart(DM_INIT_REASON_POWER_ON);
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else if (!strcmp(argv[1], "inflightrestart"))
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dm_restart(DM_INIT_REASON_IN_FLIGHT);
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else
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usage();
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@@ -38,5 +38,3 @@
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MODULE_COMMAND = dataman
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SRCS = dataman.c
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INCLUDE_DIRS += $(MAVLINK_SRC)/include/mavlink
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@@ -245,7 +245,7 @@ PARAM_DEFINE_FLOAT(FW_T_INTEG_GAIN, 0.1f);
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/**
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* Maximum vertical acceleration
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*
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* This is the maximum vertical acceleration (in metres/second^2)
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* This is the maximum vertical acceleration (in metres/second square)
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* either up or down that the controller will use to correct speed
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* or height errors. The default value of 7 m/s/s (equivalent to +- 0.7 g)
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* allows for reasonably aggressive pitch changes if required to recover
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@@ -634,13 +634,15 @@ MavlinkReceiver::handle_message_hil_sensor(mavlink_message_t *msg)
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hil_battery_status.timestamp = timestamp;
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hil_battery_status.voltage_v = 11.1f;
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hil_battery_status.voltage_filtered_v = 11.1f;
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hil_battery_status.current_a = 10.0f;
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hil_battery_status.discharged_mah = -1.0f;
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if (_battery_pub > 0) {
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orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status);
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} else {
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_baro_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
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_battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
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}
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}
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@@ -1021,6 +1021,7 @@ int sdlog2_thread_main(int argc, char *argv[])
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log_msg.body.log_SENS.baro_alt = buf.sensor.baro_alt_meter;
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log_msg.body.log_SENS.baro_temp = buf.sensor.baro_temp_celcius;
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log_msg.body.log_SENS.diff_pres = buf.sensor.differential_pressure_pa;
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log_msg.body.log_SENS.diff_pres_filtered = buf.sensor.differential_pressure_filtered_pa;
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LOGBUFFER_WRITE_AND_COUNT(SENS);
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}
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@@ -92,6 +92,7 @@ struct log_SENS_s {
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float baro_alt;
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float baro_temp;
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float diff_pres;
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float diff_pres_filtered;
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};
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/* --- LPOS - LOCAL POSITION --- */
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@@ -306,7 +307,7 @@ static const struct log_format_s log_formats[] = {
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LOG_FORMAT(ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"),
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LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"),
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LOG_FORMAT(IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"),
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LOG_FORMAT(SENS, "ffff", "BaroPres,BaroAlt,BaroTemp,DiffPres"),
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LOG_FORMAT(SENS, "fffff", "BaroPres,BaroAlt,BaroTemp,DiffPres,DiffPresFilt"),
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LOG_FORMAT(LPOS, "ffffffLLfBBB", "X,Y,Z,VX,VY,VZ,RefLat,RefLon,RefAlt,XYFlags,ZFlags,Landed"),
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LOG_FORMAT(LPSP, "ffff", "X,Y,Z,Yaw"),
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LOG_FORMAT(GPS, "QBffLLfffff", "GPSTime,FixType,EPH,EPV,Lat,Lon,Alt,VelN,VelE,VelD,Cog"),
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@@ -1031,10 +1031,11 @@ Sensors::diff_pres_poll(struct sensor_combined_s &raw)
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raw.differential_pressure_pa = _diff_pres.differential_pressure_pa;
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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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_airspeed.timestamp = hrt_absolute_time();
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_airspeed.indicated_airspeed_m_s = calc_indicated_airspeed(_diff_pres.differential_pressure_pa);
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_airspeed.true_airspeed_m_s = calc_true_airspeed(_diff_pres.differential_pressure_pa + raw.baro_pres_mbar * 1e2f,
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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, raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG);
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/* announce the airspeed if needed, just publish else */
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@@ -54,8 +54,9 @@
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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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float differential_pressure_pa; /**< Differential pressure reading */
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float max_differential_pressure_pa; /**< Maximum differential pressure reading */
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float differential_pressure_pa; /**< Differential pressure reading */
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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 */
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@@ -105,6 +105,8 @@ struct sensor_combined_s {
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float differential_pressure_pa; /**< Airspeed sensor differential pressure */
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uint64_t differential_pressure_timestamp; /**< Last measurement timestamp */
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float differential_pressure_filtered_pa; /**< Low pass filtered airspeed sensor differential pressure reading */
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};
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/**
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