Merge branch 'master' into mpc_local_pos

This commit is contained in:
Anton Babushkin
2014-04-22 11:13:11 +02:00
250 changed files with 11421 additions and 526 deletions
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2013 PX4 Development Team. All rights reserved.
* Copyright (c) 2013, 2014 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
@@ -64,9 +64,9 @@ int do_airspeed_calibration(int mavlink_fd)
{
/* give directions */
mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name);
mavlink_log_info(mavlink_fd, "don't move system");
mavlink_log_info(mavlink_fd, "ensure airspeed sensor is not registering wind");
const int calibration_count = 2500;
const int calibration_count = 2000;
int diff_pres_sub = orb_subscribe(ORB_ID(differential_pressure));
struct differential_pressure_s diff_pres;
@@ -85,13 +85,15 @@ int do_airspeed_calibration(int mavlink_fd)
if (fd > 0) {
if (OK == ioctl(fd, AIRSPEEDIOCSSCALE, (long unsigned int)&airscale)) {
paramreset_successful = true;
} else {
mavlink_log_critical(mavlink_fd, "airspeed offset zero failed");
}
close(fd);
}
if (!paramreset_successful) {
warn("WARNING: failed to set scale / offsets for airspeed sensor");
mavlink_log_critical(mavlink_fd, "could not reset dpress sensor");
warn("FAILED to set scale / offsets for airspeed");
mavlink_log_critical(mavlink_fd, "dpress reset failed");
mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name);
return ERROR;
}
@@ -107,7 +109,7 @@ int do_airspeed_calibration(int mavlink_fd)
if (poll_ret) {
orb_copy(ORB_ID(differential_pressure), diff_pres_sub, &diff_pres);
diff_pres_offset += diff_pres.differential_pressure_pa;
diff_pres_offset += diff_pres.differential_pressure_raw_pa;
calibration_counter++;
if (calibration_counter % (calibration_count / 20) == 0)
+8 -3
View File
@@ -396,6 +396,11 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe
enum VEHICLE_CMD_RESULT result = VEHICLE_CMD_RESULT_UNSUPPORTED;
bool ret = false;
/* only handle commands that are meant to be handled by this system and component */
if (cmd->target_system != status->system_id || ((cmd->target_component != status->component_id) && (cmd->target_component != 0))) { // component_id 0: valid for all components
return false;
}
/* only handle high-priority commands here */
/* request to set different system mode */
@@ -633,11 +638,11 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe
break;
default:
/* warn about unsupported commands */
/* Warn about unsupported commands, this makes sense because only commands
* to this component ID (or all) are passed by mavlink. */
answer_command(*cmd, VEHICLE_CMD_RESULT_UNSUPPORTED);
break;
}
if (result != VEHICLE_CMD_RESULT_UNSUPPORTED) {
/* already warned about unsupported commands in "default" case */
answer_command(*cmd, result);
@@ -1047,7 +1052,7 @@ int commander_thread_main(int argc, char *argv[])
orb_copy(ORB_ID(battery_status), battery_sub, &battery);
/* only consider battery voltage if system has been running 2s and battery voltage is valid */
if (status.hil_state == HIL_STATE_OFF && hrt_absolute_time() > start_time + 2000000 && battery.voltage_filtered_v > 0.0f) {
if (hrt_absolute_time() > start_time + 2000000 && battery.voltage_filtered_v > 0.0f) {
status.battery_voltage = battery.voltage_filtered_v;
status.battery_current = battery.current_a;
status.condition_battery_voltage_valid = true;
+17 -2
View File
@@ -44,7 +44,9 @@
#include <stdlib.h>
#include <fcntl.h>
#include <systemlib/systemlib.h>
#include <systemlib/err.h>
#include <queue.h>
#include <string.h>
#include "dataman.h"
@@ -594,6 +596,20 @@ task_main(int argc, char *argv[])
sem_init(&g_work_queued_sema, 1, 0);
/* See if the data manage file exists and is a multiple of the sector size */
g_task_fd = open(k_data_manager_device_path, O_RDONLY | O_BINARY);
if (g_task_fd >= 0) {
/* File exists, check its size */
int file_size = lseek(g_task_fd, 0, SEEK_END);
if ((file_size % k_sector_size) != 0) {
warnx("Incompatible data manager file %s, resetting it", k_data_manager_device_path);
close(g_task_fd);
unlink(k_data_manager_device_path);
}
else
close(g_task_fd);
}
/* Open or create the data manager file */
g_task_fd = open(k_data_manager_device_path, O_RDWR | O_CREAT | O_BINARY);
@@ -603,7 +619,7 @@ task_main(int argc, char *argv[])
return -1;
}
if (lseek(g_task_fd, max_offset, SEEK_SET) != max_offset) {
if ((unsigned)lseek(g_task_fd, max_offset, SEEK_SET) != max_offset) {
close(g_task_fd);
warnx("Could not seek data manager file %s", k_data_manager_device_path);
sem_post(&g_init_sema); /* Don't want to hang startup */
@@ -776,4 +792,3 @@ dataman_main(int argc, char *argv[])
exit(1);
}
+1 -1
View File
@@ -79,7 +79,7 @@ extern "C" {
} dm_reset_reason;
/* Maximum size in bytes of a single item instance */
#define DM_MAX_DATA_SIZE 126
#define DM_MAX_DATA_SIZE 124
/* Retrieve from the data manager store */
__EXPORT ssize_t
@@ -660,18 +660,24 @@ FixedwingAttitudeControl::task_main()
float airspeed;
/* if airspeed is smaller than min, the sensor is not giving good readings */
if ((_airspeed.indicated_airspeed_m_s < 0.5f * _parameters.airspeed_min) ||
!isfinite(_airspeed.indicated_airspeed_m_s) ||
/* if airspeed is not updating, we assume the normal average speed */
if (!isfinite(_airspeed.true_airspeed_m_s) ||
hrt_elapsed_time(&_airspeed.timestamp) > 1e6) {
airspeed = _parameters.airspeed_trim;
} else {
airspeed = _airspeed.indicated_airspeed_m_s;
airspeed = _airspeed.true_airspeed_m_s;
}
float airspeed_scaling = _parameters.airspeed_trim / airspeed;
//warnx("aspd scale: %6.2f act scale: %6.2f", airspeed_scaling, actuator_scaling);
/*
* For scaling our actuators using anything less than the min (close to stall)
* speed doesn't make any sense - its the strongest reasonable deflection we
* want to do in flight and its the baseline a human pilot would choose.
*
* Forcing the scaling to this value allows reasonable handheld tests.
*/
float airspeed_scaling = _parameters.airspeed_trim / ((airspeed < _parameters.airspeed_min) ? _parameters.airspeed_min : airspeed);
float roll_sp = _parameters.rollsp_offset_rad;
float pitch_sp = _parameters.pitchsp_offset_rad;
@@ -961,7 +961,7 @@ FixedwingEstimator::task_main()
}
// Publish results
if (_initialized) {
if (_initialized && (check == OK)) {
+73
View File
@@ -0,0 +1,73 @@
/****************************************************************************
*
* Copyright (c) 2014 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 mavlink_commands.cpp
* Mavlink commands stream implementation.
*
* @author Anton Babushkin <anton.babushkin@me.com>
*/
#include "mavlink_commands.h"
MavlinkCommandsStream::MavlinkCommandsStream(Mavlink *mavlink, mavlink_channel_t channel) : _channel(channel)
{
_cmd_sub = mavlink->add_orb_subscription(ORB_ID(vehicle_command));
_cmd = (struct vehicle_command_s *)_cmd_sub->get_data();
}
MavlinkCommandsStream::~MavlinkCommandsStream()
{
}
void
MavlinkCommandsStream::update(const hrt_abstime t)
{
if (_cmd_sub->update(t)) {
/* only send commands for other systems/components */
if (_cmd->target_system != mavlink_system.sysid || _cmd->target_component != mavlink_system.compid) {
mavlink_msg_command_long_send(_channel,
_cmd->target_system,
_cmd->target_component,
_cmd->command,
_cmd->confirmation,
_cmd->param1,
_cmd->param2,
_cmd->param3,
_cmd->param4,
_cmd->param5,
_cmd->param6,
_cmd->param7);
}
}
}
+65
View File
@@ -0,0 +1,65 @@
/****************************************************************************
*
* Copyright (c) 2014 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 mavlink_commands.h
* Mavlink commands stream definition.
*
* @author Anton Babushkin <anton.babushkin@me.com>
*/
#ifndef MAVLINK_COMMANDS_H_
#define MAVLINK_COMMANDS_H_
#include <uORB/uORB.h>
#include <uORB/topics/vehicle_command.h>
class Mavlink;
class MavlinkCommansStream;
#include "mavlink_main.h"
class MavlinkCommandsStream
{
private:
MavlinkOrbSubscription *_cmd_sub;
struct vehicle_command_s *_cmd;
mavlink_channel_t _channel;
public:
MavlinkCommandsStream(Mavlink *mavlink, mavlink_channel_t channel);
~MavlinkCommandsStream();
void update(const hrt_abstime t);
};
#endif /* MAVLINK_COMMANDS_H_ */
+220 -11
View File
@@ -81,6 +81,7 @@
#include "mavlink_messages.h"
#include "mavlink_receiver.h"
#include "mavlink_rate_limiter.h"
#include "mavlink_commands.h"
/* oddly, ERROR is not defined for c++ */
#ifdef ERROR
@@ -166,12 +167,12 @@ mavlink_send_uart_bytes(mavlink_channel_t channel, const uint8_t *ch, int length
int buf_free = 0;
if (instance->get_flow_control_enabled()
&& ioctl(uart, FIONWRITE, (unsigned long)&buf_free) == 0) {
&& ioctl(uart, FIONWRITE, (unsigned long)&buf_free) == 0) {
if (buf_free == 0) {
if (last_write_times[(unsigned)channel] != 0 &&
hrt_elapsed_time(&last_write_times[(unsigned)channel]) > 500 * 1000UL) {
hrt_elapsed_time(&last_write_times[(unsigned)channel]) > 500 * 1000UL) {
warnx("DISABLING HARDWARE FLOW CONTROL");
instance->enable_flow_control(false);
@@ -185,12 +186,17 @@ mavlink_send_uart_bytes(mavlink_channel_t channel, const uint8_t *ch, int length
}
}
ssize_t ret = write(uart, ch, desired);
if (ret != desired) {
// XXX do something here, but change to using FIONWRITE and OS buf size for detection
/* If the wait until transmit flag is on, only transmit after we've received messages.
Otherwise, transmit all the time. */
if (instance->should_transmit()) {
ssize_t ret = write(uart, ch, desired);
if (ret != desired) {
// XXX do something here, but change to using FIONWRITE and OS buf size for detection
}
}
}
static void usage(void);
@@ -203,14 +209,21 @@ Mavlink::Mavlink() :
_task_running(false),
_hil_enabled(false),
_is_usb_uart(false),
_wait_to_transmit(false),
_received_messages(false),
_main_loop_delay(1000),
_subscriptions(nullptr),
_streams(nullptr),
_mission_pub(-1),
_verbose(false),
_forwarding_on(false),
_passing_on(false),
_uart_fd(-1),
_mavlink_param_queue_index(0),
_subscribe_to_stream(nullptr),
_subscribe_to_stream_rate(0.0f),
_flow_control_enabled(true),
_message_buffer({}),
/* performance counters */
_loop_perf(perf_alloc(PC_ELAPSED, "mavlink"))
@@ -261,7 +274,6 @@ Mavlink::Mavlink() :
errx(1, "instance ID is out of range");
break;
}
}
Mavlink::~Mavlink()
@@ -394,6 +406,18 @@ Mavlink::instance_exists(const char *device_name, Mavlink *self)
return false;
}
void
Mavlink::forward_message(mavlink_message_t *msg, Mavlink *self)
{
Mavlink *inst;
LL_FOREACH(_mavlink_instances, inst) {
if (inst != self) {
inst->pass_message(msg);
}
}
}
int
Mavlink::get_uart_fd(unsigned index)
{
@@ -808,10 +832,10 @@ void Mavlink::publish_mission()
{
/* Initialize mission publication if necessary */
if (_mission_pub < 0) {
_mission_pub = orb_advertise(ORB_ID(mission), &mission);
_mission_pub = orb_advertise(ORB_ID(offboard_mission), &mission);
} else {
orb_publish(ORB_ID(mission), _mission_pub, &mission);
orb_publish(ORB_ID(offboard_mission), _mission_pub, &mission);
}
}
@@ -1616,6 +1640,125 @@ Mavlink::configure_stream_threadsafe(const char *stream_name, const float rate)
}
}
int
Mavlink::message_buffer_init(int size)
{
_message_buffer.size = size;
_message_buffer.write_ptr = 0;
_message_buffer.read_ptr = 0;
_message_buffer.data = (char*)malloc(_message_buffer.size);
return (_message_buffer.data == 0) ? ERROR : OK;
}
void
Mavlink::message_buffer_destroy()
{
_message_buffer.size = 0;
_message_buffer.write_ptr = 0;
_message_buffer.read_ptr = 0;
free(_message_buffer.data);
}
int
Mavlink::message_buffer_count()
{
int n = _message_buffer.write_ptr - _message_buffer.read_ptr;
if (n < 0) {
n += _message_buffer.size;
}
return n;
}
int
Mavlink::message_buffer_is_empty()
{
return _message_buffer.read_ptr == _message_buffer.write_ptr;
}
bool
Mavlink::message_buffer_write(void *ptr, int size)
{
// bytes available to write
int available = _message_buffer.read_ptr - _message_buffer.write_ptr - 1;
if (available < 0) {
available += _message_buffer.size;
}
if (size > available) {
// buffer overflow
return false;
}
char *c = (char *) ptr;
int n = _message_buffer.size - _message_buffer.write_ptr; // bytes to end of the buffer
if (n < size) {
// message goes over end of the buffer
memcpy(&(_message_buffer.data[_message_buffer.write_ptr]), c, n);
_message_buffer.write_ptr = 0;
} else {
n = 0;
}
// now: n = bytes already written
int p = size - n; // number of bytes to write
memcpy(&(_message_buffer.data[_message_buffer.write_ptr]), &(c[n]), p);
_message_buffer.write_ptr = (_message_buffer.write_ptr + p) % _message_buffer.size;
return true;
}
int
Mavlink::message_buffer_get_ptr(void **ptr, bool *is_part)
{
// bytes available to read
int available = _message_buffer.write_ptr - _message_buffer.read_ptr;
if (available == 0) {
return 0; // buffer is empty
}
int n = 0;
if (available > 0) {
// read pointer is before write pointer, all available bytes can be read
n = available;
*is_part = false;
} else {
// read pointer is after write pointer, read bytes from read_ptr to end of the buffer
n = _message_buffer.size - _message_buffer.read_ptr;
*is_part = _message_buffer.write_ptr > 0;
}
*ptr = &(_message_buffer.data[_message_buffer.read_ptr]);
return n;
}
void
Mavlink::message_buffer_mark_read(int n)
{
_message_buffer.read_ptr = (_message_buffer.read_ptr + n) % _message_buffer.size;
}
void
Mavlink::pass_message(mavlink_message_t *msg)
{
if (_passing_on) {
/* size is 8 bytes plus variable payload */
int size = MAVLINK_NUM_NON_PAYLOAD_BYTES + msg->len;
pthread_mutex_lock(&_message_buffer_mutex);
message_buffer_write(msg, size);
pthread_mutex_unlock(&_message_buffer_mutex);
}
}
int
Mavlink::task_main(int argc, char *argv[])
{
@@ -1632,7 +1775,7 @@ Mavlink::task_main(int argc, char *argv[])
* set error flag instead */
bool err_flag = false;
while ((ch = getopt(argc, argv, "b:r:d:m:v")) != EOF) {
while ((ch = getopt(argc, argv, "b:r:d:m:fpvw")) != EOF) {
switch (ch) {
case 'b':
_baudrate = strtoul(optarg, NULL, 10);
@@ -1672,10 +1815,22 @@ Mavlink::task_main(int argc, char *argv[])
break;
case 'f':
_forwarding_on = true;
break;
case 'p':
_passing_on = true;
break;
case 'v':
_verbose = true;
break;
case 'w':
_wait_to_transmit = true;
break;
default:
err_flag = true;
break;
@@ -1740,6 +1895,17 @@ Mavlink::task_main(int argc, char *argv[])
/* initialize mavlink text message buffering */
mavlink_logbuffer_init(&_logbuffer, 5);
/* if we are passing on mavlink messages, we need to prepare a buffer for this instance */
if (_passing_on) {
/* initialize message buffer if multiplexing is on */
if (OK != message_buffer_init(500)) {
errx(1, "can't allocate message buffer, exiting");
}
/* initialize message buffer mutex */
pthread_mutex_init(&_message_buffer_mutex, NULL);
}
/* create the device node that's used for sending text log messages, etc. */
register_driver(MAVLINK_LOG_DEVICE, &fops, 0666, NULL);
@@ -1766,6 +1932,8 @@ Mavlink::task_main(int argc, char *argv[])
struct vehicle_status_s *status = (struct vehicle_status_s *) status_sub->get_data();
MavlinkCommandsStream commands_stream(this, _channel);
/* add default streams depending on mode and intervals depending on datarate */
float rate_mult = _datarate / 1000.0f;
@@ -1783,6 +1951,9 @@ Mavlink::task_main(int argc, char *argv[])
configure_stream("LOCAL_POSITION_NED", 3.0f * rate_mult);
configure_stream("RC_CHANNELS_RAW", 1.0f * rate_mult);
configure_stream("NAMED_VALUE_FLOAT", 1.0f * rate_mult);
configure_stream("GLOBAL_POSITION_SETPOINT_INT", 3.0f * rate_mult);
configure_stream("ROLL_PITCH_YAW_THRUST_SETPOINT", 3.0f * rate_mult);
configure_stream("DISTANCE_SENSOR", 0.5f);
break;
case MAVLINK_MODE_CAMERA:
@@ -1826,6 +1997,9 @@ Mavlink::task_main(int argc, char *argv[])
set_hil_enabled(status->hil_state == HIL_STATE_ON);
}
/* update commands stream */
commands_stream.update(t);
/* check for requested subscriptions */
if (_subscribe_to_stream != nullptr) {
if (OK == configure_stream(_subscribe_to_stream, _subscribe_to_stream_rate)) {
@@ -1884,6 +2058,37 @@ Mavlink::task_main(int argc, char *argv[])
}
}
/* pass messages from other UARTs */
if (_passing_on) {
bool is_part;
void *read_ptr;
/* guard get ptr by mutex */
pthread_mutex_lock(&_message_buffer_mutex);
int available = message_buffer_get_ptr(&read_ptr, &is_part);
pthread_mutex_unlock(&_message_buffer_mutex);
if (available > 0) {
/* write first part of buffer */
_mavlink_resend_uart(_channel, (const mavlink_message_t*)read_ptr);
message_buffer_mark_read(available);
/* write second part of buffer if there is some */
if (is_part) {
/* guard get ptr by mutex */
pthread_mutex_lock(&_message_buffer_mutex);
available = message_buffer_get_ptr(&read_ptr, &is_part);
pthread_mutex_unlock(&_message_buffer_mutex);
_mavlink_resend_uart(_channel, (const mavlink_message_t*)read_ptr);
message_buffer_mark_read(available);
}
}
}
perf_end(_loop_perf);
}
@@ -1928,6 +2133,10 @@ Mavlink::task_main(int argc, char *argv[])
/* close mavlink logging device */
close(_mavlink_fd);
if (_passing_on) {
message_buffer_destroy();
pthread_mutex_destroy(&_message_buffer_mutex);
}
/* destroy log buffer */
mavlink_logbuffer_destroy(&_logbuffer);
@@ -2067,7 +2276,7 @@ Mavlink::stream(int argc, char *argv[])
static void usage()
{
warnx("usage: mavlink {start|stop-all|stream} [-d device] [-b baudrate] [-r rate] [-m mode] [-s stream] [-v]");
warnx("usage: mavlink {start|stop-all|stream} [-d device] [-b baudrate] [-r rate] [-m mode] [-s stream] [-f] [-p] [-v] [-w]");
}
int mavlink_main(int argc, char *argv[])
+47 -1
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@@ -138,6 +138,8 @@ public:
static bool instance_exists(const char *device_name, Mavlink *self);
static void forward_message(mavlink_message_t *msg, Mavlink *self);
static int get_uart_fd(unsigned index);
int get_uart_fd();
@@ -153,10 +155,12 @@ public:
void set_mode(enum MAVLINK_MODE);
enum MAVLINK_MODE get_mode() { return _mode; }
bool get_hil_enabled() { return _hil_enabled; };
bool get_hil_enabled() { return _hil_enabled; }
bool get_flow_control_enabled() { return _flow_control_enabled; }
bool get_forwarding_on() { return _forwarding_on; }
/**
* Handle waypoint related messages.
*/
@@ -196,6 +200,16 @@ public:
bool _task_should_exit; /**< if true, mavlink task should exit */
int get_mavlink_fd() { return _mavlink_fd; }
/* Functions for waiting to start transmission until message received. */
void set_has_received_messages(bool received_messages) { _received_messages = received_messages; }
bool get_has_received_messages() { return _received_messages; }
void set_wait_to_transmit(bool wait) { _wait_to_transmit = wait; }
bool get_wait_to_transmit() { return _wait_to_transmit; }
bool should_transmit() { return (!_wait_to_transmit || (_wait_to_transmit && _received_messages)); }
protected:
Mavlink *next;
@@ -210,6 +224,8 @@ private:
/* states */
bool _hil_enabled; /**< Hardware In the Loop mode */
bool _is_usb_uart; /**< Port is USB */
bool _wait_to_transmit; /**< Wait to transmit until received messages. */
bool _received_messages; /**< Whether we've received valid mavlink messages. */
unsigned _main_loop_delay; /**< mainloop delay, depends on data rate */
@@ -234,6 +250,8 @@ private:
mavlink_wpm_storage *_wpm;
bool _verbose;
bool _forwarding_on;
bool _passing_on;
int _uart_fd;
int _baudrate;
int _datarate;
@@ -252,6 +270,18 @@ private:
bool _flow_control_enabled;
struct mavlink_message_buffer {
int write_ptr;
int read_ptr;
int size;
char *data;
};
mavlink_message_buffer _message_buffer;
pthread_mutex_t _message_buffer_mutex;
/**
* Send one parameter.
*
@@ -315,6 +345,22 @@ private:
int configure_stream(const char *stream_name, const float rate);
void configure_stream_threadsafe(const char *stream_name, const float rate);
int message_buffer_init(int size);
void message_buffer_destroy();
int message_buffer_count();
int message_buffer_is_empty();
bool message_buffer_write(void *ptr, int size);
int message_buffer_get_ptr(void **ptr, bool *is_part);
void message_buffer_mark_read(int n);
void pass_message(mavlink_message_t *msg);
static int mavlink_dev_ioctl(struct file *filep, int cmd, unsigned long arg);
/**
+106 -20
View File
@@ -72,6 +72,7 @@
#include <uORB/topics/navigation_capabilities.h>
#include <drivers/drv_rc_input.h>
#include <drivers/drv_pwm_output.h>
#include <drivers/drv_range_finder.h>
#include "mavlink_messages.h"
@@ -262,22 +263,21 @@ protected:
void send(const hrt_abstime t)
{
if (status_sub->update(t)) {
mavlink_msg_sys_status_send(_channel,
status->onboard_control_sensors_present,
status->onboard_control_sensors_enabled,
status->onboard_control_sensors_health,
status->load * 1000.0f,
status->battery_voltage * 1000.0f,
status->battery_current * 1000.0f,
status->battery_remaining,
status->drop_rate_comm,
status->errors_comm,
status->errors_count1,
status->errors_count2,
status->errors_count3,
status->errors_count4);
}
status_sub->update(t);
mavlink_msg_sys_status_send(_channel,
status->onboard_control_sensors_present,
status->onboard_control_sensors_enabled,
status->onboard_control_sensors_health,
status->load * 1000.0f,
status->battery_voltage * 1000.0f,
status->battery_current * 1000.0f,
status->battery_remaining * 100.0f,
status->drop_rate_comm,
status->errors_comm,
status->errors_count1,
status->errors_count2,
status->errors_count3,
status->errors_count4);
}
};
@@ -641,6 +641,47 @@ protected:
};
class MavlinkStreamViconPositionEstimate : public MavlinkStream
{
public:
const char *get_name()
{
return "VICON_POSITION_ESTIMATE";
}
MavlinkStream *new_instance()
{
return new MavlinkStreamViconPositionEstimate();
}
private:
MavlinkOrbSubscription *pos_sub;
struct vehicle_vicon_position_s *pos;
protected:
void subscribe(Mavlink *mavlink)
{
pos_sub = mavlink->add_orb_subscription(ORB_ID(vehicle_vicon_position));
pos = (struct vehicle_vicon_position_s *)pos_sub->get_data();
}
void send(const hrt_abstime t)
{
if (pos_sub->update(t)) {
mavlink_msg_vicon_position_estimate_send(_channel,
pos->timestamp / 1000,
pos->x,
pos->y,
pos->z,
pos->roll,
pos->pitch,
pos->yaw);
}
}
};
class MavlinkStreamGPSGlobalOrigin : public MavlinkStream
{
public:
@@ -1253,8 +1294,6 @@ protected:
{
status_sub = mavlink->add_orb_subscription(ORB_ID(vehicle_status));
status = (struct vehicle_status_s *)status_sub->get_data();
}
void send(const hrt_abstime t)
@@ -1265,15 +1304,60 @@ protected:
|| status->arming_state == ARMING_STATE_ARMED_ERROR) {
/* send camera capture on */
mavlink_msg_command_long_send(_channel, 42, 30, MAV_CMD_DO_CONTROL_VIDEO, 0, 0, 0, 0, 1, 0, 0, 0);
mavlink_msg_command_long_send(_channel, mavlink_system.sysid, 0, MAV_CMD_DO_CONTROL_VIDEO, 0, 0, 0, 0, 1, 0, 0, 0);
} else {
/* send camera capture off */
mavlink_msg_command_long_send(_channel, 42, 30, MAV_CMD_DO_CONTROL_VIDEO, 0, 0, 0, 0, 0, 0, 0, 0);
mavlink_msg_command_long_send(_channel, mavlink_system.sysid, 0, MAV_CMD_DO_CONTROL_VIDEO, 0, 0, 0, 0, 0, 0, 0, 0);
}
}
};
class MavlinkStreamDistanceSensor : public MavlinkStream
{
public:
const char *get_name()
{
return "DISTANCE_SENSOR";
}
MavlinkStream *new_instance()
{
return new MavlinkStreamDistanceSensor();
}
private:
MavlinkOrbSubscription *range_sub;
struct range_finder_report *range;
protected:
void subscribe(Mavlink *mavlink)
{
range_sub = mavlink->add_orb_subscription(ORB_ID(sensor_range_finder));
range = (struct range_finder_report *)range_sub->get_data();
}
void send(const hrt_abstime t)
{
(void)range_sub->update(t);
uint8_t type;
switch (range->type) {
case RANGE_FINDER_TYPE_LASER:
type = MAV_DISTANCE_SENSOR_LASER;
break;
}
uint8_t id = 0;
uint8_t orientation = 0;
uint8_t covariance = 20;
mavlink_msg_distance_sensor_send(_channel, range->timestamp / 1000, type, id, orientation,
range->minimum_distance*100, range->maximum_distance*100, range->distance*100, covariance);
}
};
MavlinkStream *streams_list[] = {
new MavlinkStreamHeartbeat(),
new MavlinkStreamSysStatus(),
@@ -1300,5 +1384,7 @@ MavlinkStream *streams_list[] = {
new MavlinkStreamAttitudeControls(),
new MavlinkStreamNamedValueFloat(),
new MavlinkStreamCameraCapture(),
new MavlinkStreamDistanceSensor(),
new MavlinkStreamViconPositionEstimate(),
nullptr
};
+38 -31
View File
@@ -181,6 +181,10 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg)
break;
}
}
/* If we've received a valid message, mark the flag indicating so.
This is used in the '-w' command-line flag. */
_mavlink->set_has_received_messages(true);
}
void
@@ -222,12 +226,10 @@ MavlinkReceiver::handle_message_command_long(mavlink_message_t *msg)
vcmd.source_component = msg->compid;
vcmd.confirmation = cmd_mavlink.confirmation;
/* check if topic is advertised */
if (_cmd_pub <= 0) {
if (_cmd_pub < 0) {
_cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd);
} else {
/* publish */
orb_publish(ORB_ID(vehicle_command), _cmd_pub, &vcmd);
}
}
@@ -254,7 +256,7 @@ MavlinkReceiver::handle_message_optical_flow(mavlink_message_t *msg)
f.quality = flow.quality;
f.sensor_id = flow.sensor_id;
if (_flow_pub <= 0) {
if (_flow_pub < 0) {
_flow_pub = orb_advertise(ORB_ID(optical_flow), &f);
} else {
@@ -288,7 +290,7 @@ MavlinkReceiver::handle_message_set_mode(mavlink_message_t *msg)
vcmd.source_component = msg->compid;
vcmd.confirmation = 1;
if (_cmd_pub <= 0) {
if (_cmd_pub < 0) {
_cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd);
} else {
@@ -313,7 +315,7 @@ MavlinkReceiver::handle_message_vicon_position_estimate(mavlink_message_t *msg)
vicon_position.pitch = pos.pitch;
vicon_position.yaw = pos.yaw;
if (_vicon_position_pub <= 0) {
if (_vicon_position_pub < 0) {
_vicon_position_pub = orb_advertise(ORB_ID(vehicle_vicon_position), &vicon_position);
} else {
@@ -374,7 +376,7 @@ MavlinkReceiver::handle_message_quad_swarm_roll_pitch_yaw_thrust(mavlink_message
offboard_control_sp.timestamp = hrt_absolute_time();
if (_offboard_control_sp_pub <= 0) {
if (_offboard_control_sp_pub < 0) {
_offboard_control_sp_pub = orb_advertise(ORB_ID(offboard_control_setpoint), &offboard_control_sp);
} else {
@@ -402,7 +404,7 @@ MavlinkReceiver::handle_message_radio_status(mavlink_message_t *msg)
tstatus.rxerrors = rstatus.rxerrors;
tstatus.fixed = rstatus.fixed;
if (_telemetry_status_pub <= 0) {
if (_telemetry_status_pub < 0) {
_telemetry_status_pub = orb_advertise(ORB_ID(telemetry_status), &tstatus);
} else {
@@ -429,7 +431,7 @@ MavlinkReceiver::handle_message_manual_control(mavlink_message_t *msg)
rc.chan[2].scaled = man.r / 1000.0f;
rc.chan[3].scaled = man.z / 1000.0f;
if (_rc_pub == 0) {
if (_rc_pub < 0) {
_rc_pub = orb_advertise(ORB_ID(rc_channels), &rc);
} else {
@@ -451,7 +453,7 @@ MavlinkReceiver::handle_message_manual_control(mavlink_message_t *msg)
manual.yaw = man.r / 1000.0f;
manual.throttle = man.z / 1000.0f;
if (_manual_pub == 0) {
if (_manual_pub < 0) {
_manual_pub = orb_advertise(ORB_ID(manual_control_setpoint), &manual);
} else {
@@ -620,11 +622,11 @@ MavlinkReceiver::handle_message_hil_sensor(mavlink_message_t *msg)
hil_sensors.differential_pressure_timestamp = timestamp;
/* publish combined sensor topic */
if (_sensors_pub > 0) {
orb_publish(ORB_ID(sensor_combined), _sensors_pub, &hil_sensors);
if (_sensors_pub < 0) {
_sensors_pub = orb_advertise(ORB_ID(sensor_combined), &hil_sensors);
} else {
_sensors_pub = orb_advertise(ORB_ID(sensor_combined), &hil_sensors);
orb_publish(ORB_ID(sensor_combined), _sensors_pub, &hil_sensors);
}
}
@@ -639,11 +641,11 @@ MavlinkReceiver::handle_message_hil_sensor(mavlink_message_t *msg)
hil_battery_status.current_a = 10.0f;
hil_battery_status.discharged_mah = -1.0f;
if (_battery_pub > 0) {
orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status);
if (_battery_pub < 0) {
_battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
} else {
_battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status);
}
}
@@ -695,11 +697,11 @@ MavlinkReceiver::handle_message_hil_gps(mavlink_message_t *msg)
hil_gps.fix_type = gps.fix_type;
hil_gps.satellites_visible = gps.satellites_visible;
if (_gps_pub > 0) {
orb_publish(ORB_ID(vehicle_gps_position), _gps_pub, &hil_gps);
if (_gps_pub < 0) {
_gps_pub = orb_advertise(ORB_ID(vehicle_gps_position), &hil_gps);
} else {
_gps_pub = orb_advertise(ORB_ID(vehicle_gps_position), &hil_gps);
orb_publish(ORB_ID(vehicle_gps_position), _gps_pub, &hil_gps);
}
}
@@ -753,11 +755,11 @@ MavlinkReceiver::handle_message_hil_state_quaternion(mavlink_message_t *msg)
hil_attitude.pitchspeed = hil_state.pitchspeed;
hil_attitude.yawspeed = hil_state.yawspeed;
if (_attitude_pub > 0) {
orb_publish(ORB_ID(vehicle_attitude), _attitude_pub, &hil_attitude);
if (_attitude_pub < 0) {
_attitude_pub = orb_advertise(ORB_ID(vehicle_attitude), &hil_attitude);
} else {
_attitude_pub = orb_advertise(ORB_ID(vehicle_attitude), &hil_attitude);
orb_publish(ORB_ID(vehicle_attitude), _attitude_pub, &hil_attitude);
}
}
@@ -777,11 +779,11 @@ MavlinkReceiver::handle_message_hil_state_quaternion(mavlink_message_t *msg)
hil_global_pos.eph = 2.0f;
hil_global_pos.epv = 4.0f;
if (_global_pos_pub > 0) {
orb_publish(ORB_ID(vehicle_global_position), _global_pos_pub, &hil_global_pos);
if (_global_pos_pub < 0) {
_global_pos_pub = orb_advertise(ORB_ID(vehicle_global_position), &hil_global_pos);
} else {
_global_pos_pub = orb_advertise(ORB_ID(vehicle_global_position), &hil_global_pos);
orb_publish(ORB_ID(vehicle_global_position), _global_pos_pub, &hil_global_pos);
}
}
@@ -821,11 +823,11 @@ MavlinkReceiver::handle_message_hil_state_quaternion(mavlink_message_t *msg)
bool landed = (float)(hil_state.alt) / 1000.0f < (_hil_local_alt0 + 0.1f); // XXX improve?
hil_local_pos.landed = landed;
if (_local_pos_pub > 0) {
orb_publish(ORB_ID(vehicle_local_position), _local_pos_pub, &hil_local_pos);
if (_local_pos_pub < 0) {
_local_pos_pub = orb_advertise(ORB_ID(vehicle_local_position), &hil_local_pos);
} else {
_local_pos_pub = orb_advertise(ORB_ID(vehicle_local_position), &hil_local_pos);
orb_publish(ORB_ID(vehicle_local_position), _local_pos_pub, &hil_local_pos);
}
}
@@ -862,11 +864,11 @@ MavlinkReceiver::handle_message_hil_state_quaternion(mavlink_message_t *msg)
hil_battery_status.current_a = 10.0f;
hil_battery_status.discharged_mah = -1.0f;
if (_battery_pub > 0) {
orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status);
if (_battery_pub < 0) {
_battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
} else {
_battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status);
}
}
}
@@ -918,6 +920,11 @@ MavlinkReceiver::receive_thread(void *arg)
/* handle packet with parameter component */
_mavlink->mavlink_pm_message_handler(_mavlink->get_channel(), &msg);
if (_mavlink->get_forwarding_on()) {
/* forward any messages to other mavlink instances */
Mavlink::forward_message(&msg, _mavlink);
}
}
}
}
+1 -1
View File
@@ -120,7 +120,6 @@ private:
mavlink_status_t status;
struct vehicle_local_position_s hil_local_pos;
int _manual_sub;
orb_advert_t _global_pos_pub;
orb_advert_t _local_pos_pub;
orb_advert_t _attitude_pub;
@@ -139,6 +138,7 @@ private:
orb_advert_t _telemetry_status_pub;
orb_advert_t _rc_pub;
orb_advert_t _manual_pub;
int _manual_sub;
int _hil_frames;
uint64_t _old_timestamp;
bool _hil_local_proj_inited;
+1 -1
View File
@@ -32,7 +32,7 @@
****************************************************************************/
/**
* @file mavlink_stream.cpp
* @file mavlink_stream.h
* Mavlink messages stream definition.
*
* @author Anton Babushkin <anton.babushkin@me.com>
+4 -1
View File
@@ -42,6 +42,9 @@ SRCS += mavlink_main.cpp \
mavlink_orb_subscription.cpp \
mavlink_messages.cpp \
mavlink_stream.cpp \
mavlink_rate_limiter.cpp
mavlink_rate_limiter.cpp \
mavlink_commands.cpp
INCLUDE_DIRS += $(MAVLINK_SRC)/include/mavlink
MAXOPTIMIZATION = -Os
+4 -4
View File
@@ -510,7 +510,7 @@ Navigator::offboard_mission_update(bool isrotaryWing)
{
struct mission_s offboard_mission;
if (orb_copy(ORB_ID(mission), _offboard_mission_sub, &offboard_mission) == OK) {
if (orb_copy(ORB_ID(offboard_mission), _offboard_mission_sub, &offboard_mission) == OK) {
/* Check mission feasibility, for now do not handle the return value,
* however warnings are issued to the gcs via mavlink from inside the MissionFeasiblityChecker */
@@ -543,7 +543,7 @@ Navigator::onboard_mission_update()
{
struct mission_s onboard_mission;
if (orb_copy(ORB_ID(mission), _onboard_mission_sub, &onboard_mission) == OK) {
if (orb_copy(ORB_ID(onboard_mission), _onboard_mission_sub, &onboard_mission) == OK) {
_mission.set_onboard_mission_count(onboard_mission.count);
_mission.set_current_onboard_mission_index(onboard_mission.current_index);
@@ -611,7 +611,7 @@ Navigator::task_main()
* do subscriptions
*/
_global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
_offboard_mission_sub = orb_subscribe(ORB_ID(mission));
_offboard_mission_sub = orb_subscribe(ORB_ID(offboard_mission));
_onboard_mission_sub = orb_subscribe(ORB_ID(onboard_mission));
_capabilities_sub = orb_subscribe(ORB_ID(navigation_capabilities));
_vstatus_sub = orb_subscribe(ORB_ID(vehicle_status));
@@ -1539,7 +1539,7 @@ Navigator::check_mission_item_reached()
/* check yaw if defined only for rotary wing except takeoff */
float yaw_err = _wrap_pi(_mission_item.yaw - _global_pos.yaw);
if (fabsf(yaw_err) < 0.05f) { /* XXX get rid of magic number */
if (fabsf(yaw_err) < 0.2f) { /* XXX get rid of magic number */
_waypoint_yaw_reached = true;
}
@@ -864,7 +864,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
float thrust = armed.armed ? actuator.control[3] : 0.0f;
if (landed) {
if (alt_disp2 > land_disp2 && thrust > params.land_thr) {
if (alt_disp2 > land_disp2 || thrust > params.land_thr) {
landed = false;
landed_time = 0;
}
@@ -56,7 +56,7 @@ PARAM_DEFINE_FLOAT(INAV_SONAR_FILT, 0.05f);
PARAM_DEFINE_FLOAT(INAV_SONAR_ERR, 0.5f);
PARAM_DEFINE_FLOAT(INAV_LAND_T, 3.0f);
PARAM_DEFINE_FLOAT(INAV_LAND_DISP, 0.7f);
PARAM_DEFINE_FLOAT(INAV_LAND_THR, 0.3f);
PARAM_DEFINE_FLOAT(INAV_LAND_THR, 0.2f);
int parameters_init(struct position_estimator_inav_param_handles *h)
{
+94 -84
View File
@@ -134,8 +134,6 @@ controls_tick() {
perf_begin(c_gather_sbus);
bool sbus_status = (r_status_flags & PX4IO_P_STATUS_FLAGS_RC_SBUS);
bool sbus_failsafe, sbus_frame_drop;
bool sbus_updated = sbus_input(r_raw_rc_values, &r_raw_rc_count, &sbus_failsafe, &sbus_frame_drop, PX4IO_RC_INPUT_CHANNELS);
@@ -201,94 +199,104 @@ controls_tick() {
/* update RC-received timestamp */
system_state.rc_channels_timestamp_received = hrt_absolute_time();
/* do not command anything in failsafe, kick in the RC loss counter */
if (!(r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE)) {
/* update RC-received timestamp */
system_state.rc_channels_timestamp_valid = system_state.rc_channels_timestamp_received;
/* update RC-received timestamp */
system_state.rc_channels_timestamp_valid = system_state.rc_channels_timestamp_received;
/* map raw inputs to mapped inputs */
/* XXX mapping should be atomic relative to protocol */
for (unsigned i = 0; i < r_raw_rc_count; i++) {
/* map raw inputs to mapped inputs */
/* XXX mapping should be atomic relative to protocol */
for (unsigned i = 0; i < r_raw_rc_count; i++) {
/* map the input channel */
uint16_t *conf = &r_page_rc_input_config[i * PX4IO_P_RC_CONFIG_STRIDE];
/* map the input channel */
uint16_t *conf = &r_page_rc_input_config[i * PX4IO_P_RC_CONFIG_STRIDE];
if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_ENABLED) {
if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_ENABLED) {
uint16_t raw = r_raw_rc_values[i];
uint16_t raw = r_raw_rc_values[i];
int16_t scaled;
int16_t scaled;
/*
* 1) Constrain to min/max values, as later processing depends on bounds.
*/
if (raw < conf[PX4IO_P_RC_CONFIG_MIN])
raw = conf[PX4IO_P_RC_CONFIG_MIN];
if (raw > conf[PX4IO_P_RC_CONFIG_MAX])
raw = conf[PX4IO_P_RC_CONFIG_MAX];
/*
* 1) Constrain to min/max values, as later processing depends on bounds.
*/
if (raw < conf[PX4IO_P_RC_CONFIG_MIN])
raw = conf[PX4IO_P_RC_CONFIG_MIN];
if (raw > conf[PX4IO_P_RC_CONFIG_MAX])
raw = conf[PX4IO_P_RC_CONFIG_MAX];
/*
* 2) Scale around the mid point differently for lower and upper range.
*
* This is necessary as they don't share the same endpoints and slope.
*
* First normalize to 0..1 range with correct sign (below or above center),
* then scale to 20000 range (if center is an actual center, -10000..10000,
* if parameters only support half range, scale to 10000 range, e.g. if
* center == min 0..10000, if center == max -10000..0).
*
* As the min and max bounds were enforced in step 1), division by zero
* cannot occur, as for the case of center == min or center == max the if
* statement is mutually exclusive with the arithmetic NaN case.
*
* DO NOT REMOVE OR ALTER STEP 1!
*/
if (raw > (conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE])) {
scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_MAX] - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]));
/*
* 2) Scale around the mid point differently for lower and upper range.
*
* This is necessary as they don't share the same endpoints and slope.
*
* First normalize to 0..1 range with correct sign (below or above center),
* then scale to 20000 range (if center is an actual center, -10000..10000,
* if parameters only support half range, scale to 10000 range, e.g. if
* center == min 0..10000, if center == max -10000..0).
*
* As the min and max bounds were enforced in step 1), division by zero
* cannot occur, as for the case of center == min or center == max the if
* statement is mutually exclusive with the arithmetic NaN case.
*
* DO NOT REMOVE OR ALTER STEP 1!
*/
if (raw > (conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE])) {
scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_MAX] - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]));
} else if (raw < (conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE])) {
scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE] - conf[PX4IO_P_RC_CONFIG_MIN]));
} else if (raw < (conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE])) {
scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE] - conf[PX4IO_P_RC_CONFIG_MIN]));
} else {
/* in the configured dead zone, output zero */
scaled = 0;
}
} else {
/* in the configured dead zone, output zero */
scaled = 0;
}
/* invert channel if requested */
if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_REVERSE) {
scaled = -scaled;
}
/* invert channel if requested */
if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_REVERSE)
/* and update the scaled/mapped version */
unsigned mapped = conf[PX4IO_P_RC_CONFIG_ASSIGNMENT];
if (mapped < PX4IO_CONTROL_CHANNELS) {
/* invert channel if pitch - pulling the lever down means pitching up by convention */
if (mapped == 1) {
/* roll, pitch, yaw, throttle, override is the standard order */
scaled = -scaled;
/* and update the scaled/mapped version */
unsigned mapped = conf[PX4IO_P_RC_CONFIG_ASSIGNMENT];
if (mapped < PX4IO_CONTROL_CHANNELS) {
/* invert channel if pitch - pulling the lever down means pitching up by convention */
if (mapped == 1) /* roll, pitch, yaw, throttle, override is the standard order */
scaled = -scaled;
r_rc_values[mapped] = SIGNED_TO_REG(scaled);
assigned_channels |= (1 << mapped);
}
if (mapped == 3 && r_setup_rc_thr_failsafe) {
/* throttle failsafe detection */
if (((raw < conf[PX4IO_P_RC_CONFIG_MIN]) && (raw < r_setup_rc_thr_failsafe)) ||
((raw > conf[PX4IO_P_RC_CONFIG_MAX]) && (raw > r_setup_rc_thr_failsafe))) {
r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_FAILSAFE;
} else {
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FAILSAFE);
}
}
r_rc_values[mapped] = SIGNED_TO_REG(scaled);
assigned_channels |= (1 << mapped);
}
}
}
/* set un-assigned controls to zero */
for (unsigned i = 0; i < PX4IO_CONTROL_CHANNELS; i++) {
if (!(assigned_channels & (1 << i)))
r_rc_values[i] = 0;
/* set un-assigned controls to zero */
for (unsigned i = 0; i < PX4IO_CONTROL_CHANNELS; i++) {
if (!(assigned_channels & (1 << i))) {
r_rc_values[i] = 0;
}
}
/* set RC OK flag, as we got an update */
r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_OK;
/* set RC OK flag, as we got an update */
r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_OK;
/* if we have enough channels (5) to control the vehicle, the mapping is ok */
if (assigned_channels > 4) {
r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_MAPPING_OK;
} else {
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_MAPPING_OK);
}
/* if we have enough channels (5) to control the vehicle, the mapping is ok */
if (assigned_channels > 4) {
r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_MAPPING_OK;
} else {
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_MAPPING_OK);
}
/*
@@ -316,8 +324,13 @@ controls_tick() {
* Handle losing RC input
*/
/* this kicks in if the receiver is gone or the system went to failsafe */
if (rc_input_lost || (r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE)) {
/* if we are in failsafe, clear the override flag */
if (r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE) {
r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_OVERRIDE);
}
/* this kicks in if the receiver is gone, but there is not on failsafe (indicated by separate flag) */
if (rc_input_lost) {
/* Clear the RC input status flag, clear manual override flag */
r_status_flags &= ~(
PX4IO_P_STATUS_FLAGS_OVERRIDE |
@@ -326,27 +339,24 @@ controls_tick() {
/* Mark all channels as invalid, as we just lost the RX */
r_rc_valid = 0;
/* Set raw channel count to zero */
r_raw_rc_count = 0;
/* Set the RC_LOST alarm */
r_status_alarms |= PX4IO_P_STATUS_ALARMS_RC_LOST;
}
/* this kicks in if the receiver is completely gone */
if (rc_input_lost) {
/* Set channel count to zero */
r_raw_rc_count = 0;
}
/*
* Check for manual override.
*
* The PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK flag must be set, and we
* must have R/C input.
* must have R/C input (NO FAILSAFE!).
* Override is enabled if either the hardcoded channel / value combination
* is selected, or the AP has requested it.
*/
if ((r_setup_arming & PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK)) {
(r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) &&
!(r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE)) {
bool override = false;
@@ -369,10 +379,10 @@ controls_tick() {
mixer_tick();
} else {
r_status_flags &= ~PX4IO_P_STATUS_FLAGS_OVERRIDE;
r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_OVERRIDE);
}
} else {
r_status_flags &= ~PX4IO_P_STATUS_FLAGS_OVERRIDE;
r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_OVERRIDE);
}
}
+15 -13
View File
@@ -164,10 +164,10 @@
/* setup page */
#define PX4IO_PAGE_SETUP 50
#define PX4IO_P_SETUP_FEATURES 0
#define PX4IO_P_SETUP_FEATURES_SBUS1_OUT (1 << 0) /* enable S.Bus v1 output */
#define PX4IO_P_SETUP_FEATURES_SBUS2_OUT (1 << 1) /* enable S.Bus v2 output */
#define PX4IO_P_SETUP_FEATURES_PWM_RSSI (1 << 2) /* enable PWM RSSI parsing */
#define PX4IO_P_SETUP_FEATURES_ADC_RSSI (1 << 3) /* enable ADC RSSI parsing */
#define PX4IO_P_SETUP_FEATURES_SBUS1_OUT (1 << 0) /**< enable S.Bus v1 output */
#define PX4IO_P_SETUP_FEATURES_SBUS2_OUT (1 << 1) /**< enable S.Bus v2 output */
#define PX4IO_P_SETUP_FEATURES_PWM_RSSI (1 << 2) /**< enable PWM RSSI parsing */
#define PX4IO_P_SETUP_FEATURES_ADC_RSSI (1 << 3) /**< enable ADC RSSI parsing */
#define PX4IO_P_SETUP_ARMING 1 /* arming controls */
#define PX4IO_P_SETUP_ARMING_IO_ARM_OK (1 << 0) /* OK to arm the IO side */
@@ -201,13 +201,15 @@ enum { /* DSM bind states */
dsm_bind_send_pulses,
dsm_bind_reinit_uart
};
/* 8 */
#define PX4IO_P_SETUP_SET_DEBUG 9 /* debug level for IO board */
/* 8 */
#define PX4IO_P_SETUP_SET_DEBUG 9 /* debug level for IO board */
#define PX4IO_P_SETUP_REBOOT_BL 10 /* reboot IO into bootloader */
#define PX4IO_REBOOT_BL_MAGIC 14662 /* required argument for reboot (random) */
#define PX4IO_P_SETUP_REBOOT_BL 10 /* reboot IO into bootloader */
#define PX4IO_REBOOT_BL_MAGIC 14662 /* required argument for reboot (random) */
#define PX4IO_P_SETUP_CRC 11 /* get CRC of IO firmware */
#define PX4IO_P_SETUP_CRC 11 /* get CRC of IO firmware */
/* 12 occupied by CRC */
#define PX4IO_P_SETUP_RC_THR_FAILSAFE_US 13 /**< the throttle failsafe pulse length in microseconds */
/* autopilot control values, -10000..10000 */
#define PX4IO_PAGE_CONTROLS 51 /**< actuator control groups, one after the other, 8 wide */
@@ -217,10 +219,10 @@ enum { /* DSM bind states */
#define PX4IO_P_CONTROLS_GROUP_3 (PX4IO_PROTOCOL_MAX_CONTROL_COUNT * 3) /**< 0..PX4IO_PROTOCOL_MAX_CONTROL_COUNT - 1 */
#define PX4IO_P_CONTROLS_GROUP_VALID 64
#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP0 (1 << 0) /* group 0 is valid / received */
#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP1 (1 << 1) /* group 1 is valid / received */
#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP2 (1 << 2) /* group 2 is valid / received */
#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP3 (1 << 3) /* group 3 is valid / received */
#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP0 (1 << 0) /**< group 0 is valid / received */
#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP1 (1 << 1) /**< group 1 is valid / received */
#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP2 (1 << 2) /**< group 2 is valid / received */
#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP3 (1 << 3) /**< group 3 is valid / received */
/* raw text load to the mixer parser - ignores offset */
#define PX4IO_PAGE_MIXERLOAD 52
+1
View File
@@ -108,6 +108,7 @@ extern uint16_t r_page_servo_disarmed[]; /* PX4IO_PAGE_DISARMED_PWM */
#ifdef CONFIG_ARCH_BOARD_PX4IO_V1
#define r_setup_relays r_page_setup[PX4IO_P_SETUP_RELAYS]
#endif
#define r_setup_rc_thr_failsafe r_page_setup[PX4IO_P_SETUP_RC_THR_FAILSAFE_US]
#define r_control_values (&r_page_controls[0])
+1
View File
@@ -169,6 +169,7 @@ volatile uint16_t r_page_setup[] =
[PX4IO_P_SETUP_SET_DEBUG] = 0,
[PX4IO_P_SETUP_REBOOT_BL] = 0,
[PX4IO_P_SETUP_CRC ... (PX4IO_P_SETUP_CRC+1)] = 0,
[PX4IO_P_SETUP_RC_THR_FAILSAFE_US] = 0,
};
#ifdef CONFIG_ARCH_BOARD_PX4IO_V2
+50 -26
View File
@@ -84,6 +84,8 @@
#include <uORB/topics/esc_status.h>
#include <uORB/topics/telemetry_status.h>
#include <uORB/topics/estimator_status.h>
#include <uORB/topics/system_power.h>
#include <uORB/topics/servorail_status.h>
#include <systemlib/systemlib.h>
#include <systemlib/param/param.h>
@@ -224,11 +226,11 @@ sdlog2_usage(const char *reason)
}
errx(1, "usage: sdlog2 {start|stop|status} [-r <log rate>] [-b <buffer size>] -e -a -t\n"
"\t-r\tLog rate in Hz, 0 means unlimited rate\n"
"\t-b\tLog buffer size in KiB, default is 8\n"
"\t-e\tEnable logging by default (if not, can be started by command)\n"
"\t-a\tLog only when armed (can be still overriden by command)\n"
"\t-t\tUse date/time for naming log directories and files\n");
"\t-r\tLog rate in Hz, 0 means unlimited rate\n"
"\t-b\tLog buffer size in KiB, default is 8\n"
"\t-e\tEnable logging by default (if not, can be started by command)\n"
"\t-a\tLog only when armed (can be still overriden by command)\n"
"\t-t\tUse date/time for naming log directories and files\n");
}
/**
@@ -255,11 +257,11 @@ int sdlog2_main(int argc, char *argv[])
main_thread_should_exit = false;
deamon_task = task_spawn_cmd("sdlog2",
SCHED_DEFAULT,
SCHED_PRIORITY_DEFAULT - 30,
3000,
sdlog2_thread_main,
(const char **)argv);
SCHED_DEFAULT,
SCHED_PRIORITY_DEFAULT - 30,
3000,
sdlog2_thread_main,
(const char **)argv);
exit(0);
}
@@ -796,6 +798,8 @@ int sdlog2_thread_main(int argc, char *argv[])
struct telemetry_status_s telemetry;
struct range_finder_report range_finder;
struct estimator_status_report estimator_status;
struct system_power_s system_power;
struct servorail_status_s servorail_status;
} buf;
memset(&buf, 0, sizeof(buf));
@@ -828,6 +832,8 @@ int sdlog2_thread_main(int argc, char *argv[])
struct log_DIST_s log_DIST;
struct log_TELE_s log_TELE;
struct log_ESTM_s log_ESTM;
struct log_PWR_s log_PWR;
struct log_VICN_s log_VICN;
} body;
} log_msg = {
LOG_PACKET_HEADER_INIT(0)
@@ -859,6 +865,8 @@ int sdlog2_thread_main(int argc, char *argv[])
int telemetry_sub;
int range_finder_sub;
int estimator_status_sub;
int system_power_sub;
int servorail_status_sub;
} subs;
subs.cmd_sub = orb_subscribe(ORB_ID(vehicle_command));
@@ -884,6 +892,8 @@ int sdlog2_thread_main(int argc, char *argv[])
subs.telemetry_sub = orb_subscribe(ORB_ID(telemetry_status));
subs.range_finder_sub = orb_subscribe(ORB_ID(sensor_range_finder));
subs.estimator_status_sub = orb_subscribe(ORB_ID(estimator_status));
subs.system_power_sub = orb_subscribe(ORB_ID(system_power));
subs.servorail_status_sub = orb_subscribe(ORB_ID(servorail_status));
thread_running = true;
@@ -898,9 +908,6 @@ int sdlog2_thread_main(int argc, char *argv[])
hrt_abstime barometer_timestamp = 0;
hrt_abstime differential_pressure_timestamp = 0;
/* track changes in distance status */
bool dist_bottom_present = false;
/* enable logging on start if needed */
if (log_on_start) {
/* check GPS topic to get GPS time */
@@ -1089,6 +1096,8 @@ int sdlog2_thread_main(int argc, char *argv[])
log_msg.body.log_LPOS.x = buf.local_pos.x;
log_msg.body.log_LPOS.y = buf.local_pos.y;
log_msg.body.log_LPOS.z = buf.local_pos.z;
log_msg.body.log_LPOS.ground_dist = buf.local_pos.dist_bottom;
log_msg.body.log_LPOS.ground_dist_rate = buf.local_pos.dist_bottom_rate;
log_msg.body.log_LPOS.vx = buf.local_pos.vx;
log_msg.body.log_LPOS.vy = buf.local_pos.vy;
log_msg.body.log_LPOS.vz = buf.local_pos.vz;
@@ -1098,19 +1107,8 @@ int sdlog2_thread_main(int argc, char *argv[])
log_msg.body.log_LPOS.xy_flags = (buf.local_pos.xy_valid ? 1 : 0) | (buf.local_pos.v_xy_valid ? 2 : 0) | (buf.local_pos.xy_global ? 8 : 0);
log_msg.body.log_LPOS.z_flags = (buf.local_pos.z_valid ? 1 : 0) | (buf.local_pos.v_z_valid ? 2 : 0) | (buf.local_pos.z_global ? 8 : 0);
log_msg.body.log_LPOS.landed = buf.local_pos.landed;
log_msg.body.log_LPOS.ground_dist_flags = (buf.local_pos.dist_bottom_valid ? 1 : 0);
LOGBUFFER_WRITE_AND_COUNT(LPOS);
if (buf.local_pos.dist_bottom_valid) {
dist_bottom_present = true;
}
if (dist_bottom_present) {
log_msg.msg_type = LOG_DIST_MSG;
log_msg.body.log_DIST.bottom = buf.local_pos.dist_bottom;
log_msg.body.log_DIST.bottom_rate = buf.local_pos.dist_bottom_rate;
log_msg.body.log_DIST.flags = (buf.local_pos.dist_bottom_valid ? 1 : 0);
LOGBUFFER_WRITE_AND_COUNT(DIST);
}
}
/* --- LOCAL POSITION SETPOINT --- */
@@ -1154,7 +1152,14 @@ int sdlog2_thread_main(int argc, char *argv[])
/* --- VICON POSITION --- */
if (copy_if_updated(ORB_ID(vehicle_vicon_position), subs.vicon_pos_sub, &buf.vicon_pos)) {
// TODO not implemented yet
log_msg.msg_type = LOG_VICN_MSG;
log_msg.body.log_VICN.x = buf.vicon_pos.x;
log_msg.body.log_VICN.y = buf.vicon_pos.y;
log_msg.body.log_VICN.z = buf.vicon_pos.z;
log_msg.body.log_VICN.pitch = buf.vicon_pos.pitch;
log_msg.body.log_VICN.roll = buf.vicon_pos.roll;
log_msg.body.log_VICN.yaw = buf.vicon_pos.yaw;
LOGBUFFER_WRITE_AND_COUNT(VICN);
}
/* --- FLOW --- */
@@ -1184,6 +1189,7 @@ int sdlog2_thread_main(int argc, char *argv[])
log_msg.msg_type = LOG_AIRS_MSG;
log_msg.body.log_AIRS.indicated_airspeed = buf.airspeed.indicated_airspeed_m_s;
log_msg.body.log_AIRS.true_airspeed = buf.airspeed.true_airspeed_m_s;
log_msg.body.log_AIRS.air_temperature_celsius = buf.airspeed.air_temperature_celsius;
LOGBUFFER_WRITE_AND_COUNT(AIRS);
}
@@ -1226,6 +1232,24 @@ int sdlog2_thread_main(int argc, char *argv[])
LOGBUFFER_WRITE_AND_COUNT(BATT);
}
/* --- SYSTEM POWER RAILS --- */
if (copy_if_updated(ORB_ID(system_power), subs.system_power_sub, &buf.system_power)) {
log_msg.msg_type = LOG_PWR_MSG;
log_msg.body.log_PWR.peripherals_5v = buf.system_power.voltage5V_v;
log_msg.body.log_PWR.usb_ok = buf.system_power.usb_connected;
log_msg.body.log_PWR.brick_ok = buf.system_power.brick_valid;
log_msg.body.log_PWR.servo_ok = buf.system_power.servo_valid;
log_msg.body.log_PWR.low_power_rail_overcurrent = buf.system_power.periph_5V_OC;
log_msg.body.log_PWR.high_power_rail_overcurrent = buf.system_power.hipower_5V_OC;
/* copy servo rail status topic here too */
orb_copy(ORB_ID(servorail_status), subs.servorail_status_sub, &buf.servorail_status);
log_msg.body.log_PWR.servo_rail_5v = buf.servorail_status.voltage_v;
log_msg.body.log_PWR.servo_rssi = buf.servorail_status.rssi_v;
LOGBUFFER_WRITE_AND_COUNT(PWR);
}
/* --- TELEMETRY --- */
if (copy_if_updated(ORB_ID(telemetry_status), subs.telemetry_sub, &buf.telemetry)) {
log_msg.msg_type = LOG_TELE_MSG;
+65 -43
View File
@@ -101,6 +101,8 @@ struct log_LPOS_s {
float x;
float y;
float z;
float ground_dist;
float ground_dist_rate;
float vx;
float vy;
float vz;
@@ -110,6 +112,7 @@ struct log_LPOS_s {
uint8_t xy_flags;
uint8_t z_flags;
uint8_t landed;
uint8_t ground_dist_flags;
};
/* --- LPSP - LOCAL POSITION SETPOINT --- */
@@ -174,6 +177,7 @@ struct log_OUT0_s {
struct log_AIRS_s {
float indicated_airspeed;
float true_airspeed;
float air_temperature_celsius;
};
/* --- ARSP - ATTITUDE RATE SET POINT --- */
@@ -277,6 +281,40 @@ struct log_TELE_s {
uint8_t txbuf;
};
/* --- ESTM - ESTIMATOR STATUS --- */
#define LOG_ESTM_MSG 23
struct log_ESTM_s {
float s[10];
uint8_t n_states;
uint8_t states_nan;
uint8_t covariance_nan;
uint8_t kalman_gain_nan;
};
/* --- PWR - ONBOARD POWER SYSTEM --- */
#define LOG_PWR_MSG 24
struct log_PWR_s {
float peripherals_5v;
float servo_rail_5v;
float servo_rssi;
uint8_t usb_ok;
uint8_t brick_ok;
uint8_t servo_ok;
uint8_t low_power_rail_overcurrent;
uint8_t high_power_rail_overcurrent;
};
/* --- VICN - VICON POSITION --- */
#define LOG_VICN_MSG 25
struct log_VICN_s {
float x;
float y;
float z;
float roll;
float pitch;
float yaw;
};
/********** SYSTEM MESSAGES, ID > 0x80 **********/
/* --- TIME - TIME STAMP --- */
@@ -299,59 +337,43 @@ struct log_PARM_s {
float value;
};
/* --- ESTM - ESTIMATOR STATUS --- */
#define LOG_ESTM_MSG 132
struct log_ESTM_s {
float s[10];
uint8_t n_states;
uint8_t states_nan;
uint8_t covariance_nan;
uint8_t kalman_gain_nan;
};
// struct log_ESTM_s {
// float s[32];
// uint8_t n_states;
// uint8_t states_nan;
// uint8_t covariance_nan;
// uint8_t kalman_gain_nan;
// };
#pragma pack(pop)
/* construct list of all message formats */
static const struct log_format_s log_formats[] = {
/* business-level messages, ID < 0x80 */
LOG_FORMAT(ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"),
LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"),
LOG_FORMAT(IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"),
LOG_FORMAT(SENS, "fffff", "BaroPres,BaroAlt,BaroTemp,DiffPres,DiffPresFilt"),
LOG_FORMAT(LPOS, "ffffffLLfBBB", "X,Y,Z,VX,VY,VZ,RefLat,RefLon,RefAlt,XYFlags,ZFlags,Landed"),
LOG_FORMAT(LPSP, "ffff", "X,Y,Z,Yaw"),
LOG_FORMAT(GPS, "QBffLLfffff", "GPSTime,FixType,EPH,EPV,Lat,Lon,Alt,VelN,VelE,VelD,Cog"),
LOG_FORMAT(ATTC, "ffff", "Roll,Pitch,Yaw,Thrust"),
LOG_FORMAT(STAT, "BBfBB", "MainState,ArmState,BatRem,BatWarn,Landed"),
LOG_FORMAT(RC, "ffffffffB", "Ch0,Ch1,Ch2,Ch3,Ch4,Ch5,Ch6,Ch7,Count"),
LOG_FORMAT(OUT0, "ffffffff", "Out0,Out1,Out2,Out3,Out4,Out5,Out6,Out7"),
LOG_FORMAT(AIRS, "ff", "IndSpeed,TrueSpeed"),
LOG_FORMAT(ARSP, "fff", "RollRateSP,PitchRateSP,YawRateSP"),
LOG_FORMAT(FLOW, "hhfffBB", "RawX,RawY,CompX,CompY,Dist,Q,SensID"),
LOG_FORMAT(GPOS, "LLffffff", "Lat,Lon,Alt,VelN,VelE,VelD,EPH,EPV"),
LOG_FORMAT(GPSP, "BLLffBfbf", "NavState,Lat,Lon,Alt,Yaw,Type,LoitR,LoitDir,PitMin"),
LOG_FORMAT(ESC, "HBBBHHHHHHfH", "Counter,NumESC,Conn,N,Ver,Adr,Volt,Amp,RPM,Temp,SetP,SetPRAW"),
LOG_FORMAT(GVSP, "fff", "VX,VY,VZ"),
LOG_FORMAT(BATT, "ffff", "V,VFilt,C,Discharged"),
LOG_FORMAT(DIST, "ffB", "Bottom,BottomRate,Flags"),
LOG_FORMAT(TELE, "BBBBHHB", "RSSI,RemRSSI,Noise,RemNoise,RXErr,Fixed,TXBuf"),
LOG_FORMAT(ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"),
LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"),
LOG_FORMAT(IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"),
LOG_FORMAT(SENS, "fffff", "BaroPres,BaroAlt,BaroTemp,DiffPres,DiffPresFilt"),
LOG_FORMAT(LPOS, "ffffffffLLfBBBB", "X,Y,Z,dist,distR,VX,VY,VZ,RLat,RLon,RAlt,XYFlg,ZFlg,LFlg,GFlg"),
LOG_FORMAT(LPSP, "ffff", "X,Y,Z,Yaw"),
LOG_FORMAT(GPS, "QBffLLfffff", "GPSTime,FixType,EPH,EPV,Lat,Lon,Alt,VelN,VelE,VelD,Cog"),
LOG_FORMAT(ATTC, "ffff", "Roll,Pitch,Yaw,Thrust"),
LOG_FORMAT(STAT, "BBfBB", "MainState,ArmState,BatRem,BatWarn,Landed"),
LOG_FORMAT(RC, "ffffffffB", "Ch0,Ch1,Ch2,Ch3,Ch4,Ch5,Ch6,Ch7,Count"),
LOG_FORMAT(OUT0, "ffffffff", "Out0,Out1,Out2,Out3,Out4,Out5,Out6,Out7"),
LOG_FORMAT(AIRS, "fff", "IndSpeed,TrueSpeed,AirTemp"),
LOG_FORMAT(ARSP, "fff", "RollRateSP,PitchRateSP,YawRateSP"),
LOG_FORMAT(FLOW, "hhfffBB", "RawX,RawY,CompX,CompY,Dist,Q,SensID"),
LOG_FORMAT(GPOS, "LLffffff", "Lat,Lon,Alt,VelN,VelE,VelD,EPH,EPV"),
LOG_FORMAT(GPSP, "BLLffBfbf", "NavState,Lat,Lon,Alt,Yaw,Type,LoitR,LoitDir,PitMin"),
LOG_FORMAT(ESC, "HBBBHHHHHHfH", "count,nESC,Conn,N,Ver,Adr,Volt,Amp,RPM,Temp,SetP,SetPRAW"),
LOG_FORMAT(GVSP, "fff", "VX,VY,VZ"),
LOG_FORMAT(BATT, "ffff", "V,VFilt,C,Discharged"),
LOG_FORMAT(DIST, "ffB", "Bottom,BottomRate,Flags"),
LOG_FORMAT(TELE, "BBBBHHB", "RSSI,RemRSSI,Noise,RemNoise,RXErr,Fixed,TXBuf"),
LOG_FORMAT(ESTM, "ffffffffffBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,nStat,statNaN,covNaN,kGainNaN"),
LOG_FORMAT(PWR, "fffBBBBB", "Periph5V,Servo5V,RSSI,UsbOk,BrickOk,ServoOk,PeriphOC,HipwrOC"),
LOG_FORMAT(VICN, "ffffff", "X,Y,Z,Roll,Pitch,Yaw"),
/* system-level messages, ID >= 0x80 */
// FMT: don't write format of format message, it's useless
/* FMT: don't write format of format message, it's useless */
LOG_FORMAT(TIME, "Q", "StartTime"),
LOG_FORMAT(VER, "NZ", "Arch,FwGit"),
LOG_FORMAT(PARM, "Nf", "Name,Value"),
LOG_FORMAT(ESTM, "ffffffffffBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,n_states,states_nan,cov_nan,kgain_nan"),
//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"),
LOG_FORMAT(PARM, "Nf", "Name,Value")
};
static const int log_formats_num = sizeof(log_formats) / sizeof(struct log_format_s);
static const unsigned log_formats_num = sizeof(log_formats) / sizeof(log_formats[0]);
#endif /* SDLOG2_MESSAGES_H_ */
+3 -25
View File
@@ -668,33 +668,11 @@ PARAM_DEFINE_FLOAT(RC_SCALE_PITCH, 0.6f);
*/
PARAM_DEFINE_FLOAT(RC_SCALE_YAW, 2.0f);
/**
* Failsafe channel mapping.
*
* @min 0
* @max 18
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_FS_CH, 0);
/**
* Failsafe channel mode.
*
* 0 = too low means signal loss,
* 1 = too high means signal loss
*
* @min 0
* @max 1
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_FS_MODE, 0);
/**
* Failsafe channel PWM threshold.
*
* @min 0
* @max 1
* @min 800
* @max 2200
* @group Radio Calibration
*/
PARAM_DEFINE_FLOAT(RC_FS_THR, 800);
PARAM_DEFINE_INT32(RC_FAILS_THR, 0);
+12 -23
View File
@@ -263,9 +263,7 @@ private:
float rc_scale_yaw;
float rc_scale_flaps;
int rc_fs_ch;
int rc_fs_mode;
float rc_fs_thr;
int32_t rc_fs_thr;
float battery_voltage_scaling;
float battery_current_scaling;
@@ -313,8 +311,6 @@ private:
param_t rc_scale_yaw;
param_t rc_scale_flaps;
param_t rc_fs_ch;
param_t rc_fs_mode;
param_t rc_fs_thr;
param_t battery_voltage_scaling;
@@ -531,9 +527,7 @@ Sensors::Sensors() :
_parameter_handles.rc_scale_flaps = param_find("RC_SCALE_FLAPS");
/* RC failsafe */
_parameter_handles.rc_fs_ch = param_find("RC_FS_CH");
_parameter_handles.rc_fs_mode = param_find("RC_FS_MODE");
_parameter_handles.rc_fs_thr = param_find("RC_FS_THR");
_parameter_handles.rc_fs_thr = param_find("RC_FAILS_THR");
/* gyro offsets */
_parameter_handles.gyro_offset[0] = param_find("SENS_GYRO_XOFF");
@@ -689,8 +683,6 @@ Sensors::parameters_update()
param_get(_parameter_handles.rc_scale_pitch, &(_parameters.rc_scale_pitch));
param_get(_parameter_handles.rc_scale_yaw, &(_parameters.rc_scale_yaw));
param_get(_parameter_handles.rc_scale_flaps, &(_parameters.rc_scale_flaps));
param_get(_parameter_handles.rc_fs_ch, &(_parameters.rc_fs_ch));
param_get(_parameter_handles.rc_fs_mode, &(_parameters.rc_fs_mode));
param_get(_parameter_handles.rc_fs_thr, &(_parameters.rc_fs_thr));
/* update RC function mappings */
@@ -1033,12 +1025,13 @@ Sensors::diff_pres_poll(struct sensor_combined_s &raw)
raw.differential_pressure_timestamp = _diff_pres.timestamp;
raw.differential_pressure_filtered_pa = _diff_pres.differential_pressure_filtered_pa;
float air_temperature_celcius = (_diff_pres.temperature > -300.0f) ? _diff_pres.temperature : (raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG);
float air_temperature_celsius = (_diff_pres.temperature > -300.0f) ? _diff_pres.temperature : (raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG);
_airspeed.timestamp = _diff_pres.timestamp;
_airspeed.indicated_airspeed_m_s = calc_indicated_airspeed(_diff_pres.differential_pressure_filtered_pa);
_airspeed.true_airspeed_m_s = calc_true_airspeed(_diff_pres.differential_pressure_filtered_pa + raw.baro_pres_mbar * 1e2f,
raw.baro_pres_mbar * 1e2f, air_temperature_celcius);
raw.baro_pres_mbar * 1e2f, air_temperature_celsius);
_airspeed.air_temperature_celsius = air_temperature_celsius;
/* announce the airspeed if needed, just publish else */
if (_airspeed_pub > 0) {
@@ -1312,19 +1305,15 @@ Sensors::rc_poll()
manual_control.aux5 = NAN;
/* require at least four channels to consider the signal valid */
if (rc_input.channel_count < 4)
if (rc_input.channel_count < 4) {
return;
}
/* failsafe check */
if (_parameters.rc_fs_ch != 0) {
if (_parameters.rc_fs_mode == 0) {
if (rc_input.values[_parameters.rc_fs_ch - 1] < _parameters.rc_fs_thr)
return;
} else if (_parameters.rc_fs_mode == 1) {
if (rc_input.values[_parameters.rc_fs_ch - 1] > _parameters.rc_fs_thr)
return;
}
/* check for failsafe */
if ((rc_input.rc_failsafe) || ((_parameters.rc_fs_thr != 0) && (((rc_input.values[_rc.function[THROTTLE]] < _parameters.min[_rc.function[THROTTLE]]) && (rc_input.values[_rc.function[THROTTLE]] < _parameters.rc_fs_thr))
|| ((rc_input.values[_rc.function[THROTTLE]] > _parameters.max[_rc.function[THROTTLE]]) && (rc_input.values[_rc.function[THROTTLE]] > _parameters.rc_fs_thr))))) {
/* do not publish manual control setpoints when there are none */
return;
}
unsigned channel_limit = rc_input.channel_count;
+4 -1
View File
@@ -90,6 +90,9 @@ ORB_DEFINE(battery_status, struct battery_status_s);
#include "topics/servorail_status.h"
ORB_DEFINE(servorail_status, struct servorail_status_s);
#include "topics/system_power.h"
ORB_DEFINE(system_power, struct system_power_s);
#include "topics/vehicle_global_position.h"
ORB_DEFINE(vehicle_global_position, struct vehicle_global_position_s);
@@ -124,7 +127,7 @@ ORB_DEFINE(position_setpoint_triplet, struct position_setpoint_triplet_s);
ORB_DEFINE(vehicle_global_velocity_setpoint, struct vehicle_global_velocity_setpoint_s);
#include "topics/mission.h"
ORB_DEFINE(mission, struct mission_s);
ORB_DEFINE(offboard_mission, struct mission_s);
ORB_DEFINE(onboard_mission, struct mission_s);
#include "topics/mission_result.h"
+3 -2
View File
@@ -52,9 +52,10 @@
* Airspeed
*/
struct airspeed_s {
uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
float indicated_airspeed_m_s; /**< indicated airspeed in meters per second, -1 if unknown */
float true_airspeed_m_s; /**< true airspeed in meters per second, -1 if unknown */
float true_airspeed_m_s; /**< true airspeed in meters per second, -1 if unknown */
float air_temperature_celsius; /**< air temperature in degrees celsius, -1000 if unknown */
};
/**
@@ -52,13 +52,14 @@
* Differential pressure.
*/
struct differential_pressure_s {
uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
uint64_t error_count;
uint64_t timestamp; /**< Microseconds since system boot, needed to integrate */
uint64_t error_count; /**< Number of errors detected by driver */
float differential_pressure_pa; /**< Differential pressure reading */
float differential_pressure_raw_pa; /**< Raw differential pressure reading (may be negative) */
float differential_pressure_filtered_pa; /**< Low pass filtered differential pressure reading */
float max_differential_pressure_pa; /**< Maximum differential pressure reading */
float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */
float temperature; /**< Temperature provided by sensor, -1000.0f if unknown */
float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */
float temperature; /**< Temperature provided by sensor, -1000.0f if unknown */
};
+1 -1
View File
@@ -105,7 +105,7 @@ struct mission_s
*/
/* register this as object request broker structure */
ORB_DECLARE(mission);
ORB_DECLARE(offboard_mission);
ORB_DECLARE(onboard_mission);
#endif
+71
View File
@@ -0,0 +1,71 @@
/****************************************************************************
*
* Copyright (C) 2012-2013 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 system_power.h
*
* Definition of the system_power voltage and power status uORB topic.
*/
#ifndef SYSTEM_POWER_H_
#define SYSTEM_POWER_H_
#include "../uORB.h"
#include <stdint.h>
/**
* @addtogroup topics
* @{
*/
/**
* voltage and power supply status
*/
struct system_power_s {
uint64_t timestamp; /**< microseconds since system boot */
float voltage5V_v; /**< peripheral 5V rail voltage */
uint8_t usb_connected:1; /**< USB is connected when 1 */
uint8_t brick_valid:1; /**< brick power is good when 1 */
uint8_t servo_valid:1; /**< servo power is good when 1 */
uint8_t periph_5V_OC:1; /**< peripheral overcurrent when 1 */
uint8_t hipower_5V_OC:1; /**< hi power peripheral overcurrent when 1 */
};
/**
* @}
*/
/* register this as object request broker structure */
ORB_DECLARE(system_power);
#endif