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px4-firmware
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Merge remote-tracking branch 'upstream/master' into mavlinkexternalsetpoints

This commit is contained in:
Thomas Gubler 2014-06-27 14:16:51 +02:00
parent 9f3758582f f3a77705a7
commit 038f4f6203
10 changed files with 97 additions and 68 deletions
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12
src/drivers/px4io/px4io.cpp
View File

@ -197,8 +197,10 @@ public:
* Print IO status.
*
* Print all relevant IO status information
*
* @param extended_status Shows more verbose information (in particular RC config)
*/
void print_status();
void print_status(bool extended_status);
/**
* Fetch and print debug console output.
@ -1850,7 +1852,7 @@ PX4IO::mixer_send(const char *buf, unsigned buflen, unsigned retries)
}
void
PX4IO::print_status()
PX4IO::print_status(bool extended_status)
{
/* basic configuration */
printf("protocol %u hardware %u bootloader %u buffer %uB crc 0x%04x%04x\n",
@ -2013,6 +2015,7 @@ PX4IO::print_status()
printf("\n");
}
if (extended_status) {
for (unsigned i = 0; i < _max_rc_input; i++) {
unsigned base = PX4IO_P_RC_CONFIG_STRIDE * i;
uint16_t options = io_reg_get(PX4IO_PAGE_RC_CONFIG, base + PX4IO_P_RC_CONFIG_OPTIONS);
@ -2027,6 +2030,7 @@ PX4IO::print_status()
((options & PX4IO_P_RC_CONFIG_OPTIONS_ENABLED) ? " ENABLED" : ""),
((options & PX4IO_P_RC_CONFIG_OPTIONS_REVERSE) ? " REVERSED" : ""));
}
}
printf("failsafe");
@ -2853,7 +2857,7 @@ monitor(void)
if (g_dev != nullptr) {
printf("\033[2J\033[H"); /* move cursor home and clear screen */
(void)g_dev->print_status();
(void)g_dev->print_status(false);
(void)g_dev->print_debug();
printf("\n\n\n[ Use 'px4io debug <N>' for more output. Hit <enter> three times to exit monitor mode ]\n");
@ -3119,7 +3123,7 @@ px4io_main(int argc, char *argv[])
if (!strcmp(argv[1], "status")) {
printf("[px4io] loaded\n");
g_dev->print_status();
g_dev->print_status(true);
exit(0);
}

20
src/modules/commander/commander.cpp
View File

@ -412,7 +412,7 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe
/* if HIL got enabled, reset battery status state */
if (hil_ret == OK && status->hil_state == HIL_STATE_ON) {
/* reset the arming mode to disarmed */
arming_res = arming_state_transition(status, safety, ARMING_STATE_STANDBY, armed);
arming_res = arming_state_transition(status, safety, ARMING_STATE_STANDBY, armed, mavlink_fd);
if (arming_res != TRANSITION_DENIED) {
mavlink_log_info(mavlink_fd, "[cmd] HIL: Reset ARMED state to standby");
@ -945,8 +945,8 @@ int commander_thread_main(int argc, char *argv[])
if (status.hil_state == HIL_STATE_OFF && safety.safety_switch_available && !safety.safety_off && armed.armed) {
arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY : ARMING_STATE_STANDBY_ERROR);
if (TRANSITION_CHANGED == arming_state_transition(&status, &safety, new_arming_state, &armed)) {
mavlink_log_info(mavlink_fd, "[cmd] DISARMED by safety switch");
if (TRANSITION_CHANGED == arming_state_transition(&status, &safety, new_arming_state, &armed, mavlink_fd)) {
mavlink_log_info(mavlink_fd, "#audio DISARMED by safety switch");
}
}
}
@ -1149,10 +1149,10 @@ int commander_thread_main(int argc, char *argv[])
status.battery_warning = VEHICLE_BATTERY_WARNING_CRITICAL;
if (armed.armed) {
arming_state_transition(&status, &safety, ARMING_STATE_ARMED_ERROR, &armed);
arming_state_transition(&status, &safety, ARMING_STATE_ARMED_ERROR, &armed, mavlink_fd);
} else {
arming_state_transition(&status, &safety, ARMING_STATE_STANDBY_ERROR, &armed);
arming_state_transition(&status, &safety, ARMING_STATE_STANDBY_ERROR, &armed, mavlink_fd);
}
status_changed = true;
@ -1163,7 +1163,7 @@ int commander_thread_main(int argc, char *argv[])
/* If in INIT state, try to proceed to STANDBY state */
if (status.arming_state == ARMING_STATE_INIT && low_prio_task == LOW_PRIO_TASK_NONE) {
// XXX check for sensors
arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed);
arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed, mavlink_fd);
} else {
// XXX: Add emergency stuff if sensors are lost
@ -1217,7 +1217,7 @@ int commander_thread_main(int argc, char *argv[])
if (stick_off_counter > STICK_ON_OFF_COUNTER_LIMIT) {
/* disarm to STANDBY if ARMED or to STANDBY_ERROR if ARMED_ERROR */
arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY : ARMING_STATE_STANDBY_ERROR);
arming_res = arming_state_transition(&status, &safety, new_arming_state, &armed);
arming_res = arming_state_transition(&status, &safety, new_arming_state, &armed, mavlink_fd);
stick_off_counter = 0;
} else {
@ -1239,7 +1239,7 @@ int commander_thread_main(int argc, char *argv[])
print_reject_arm("#audio: NOT ARMING: Switch to MANUAL mode first.");
} else {
arming_res = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed);
arming_res = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed, mavlink_fd);
}
stick_on_counter = 0;
@ -1941,7 +1941,7 @@ void *commander_low_prio_loop(void *arg)
/* try to go to INIT/PREFLIGHT arming state */
// XXX disable interrupts in arming_state_transition
if (TRANSITION_DENIED == arming_state_transition(&status, &safety, ARMING_STATE_INIT, &armed)) {
if (TRANSITION_DENIED == arming_state_transition(&status, &safety, ARMING_STATE_INIT, &armed, mavlink_fd)) {
answer_command(cmd, VEHICLE_CMD_RESULT_DENIED);
break;
}
@ -2004,7 +2004,7 @@ void *commander_low_prio_loop(void *arg)
tune_negative(true);
}
arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed);
arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed, mavlink_fd);
break;
}

2
src/modules/commander/state_machine_helper.h
View File

@ -57,7 +57,7 @@ typedef enum {
} transition_result_t;
transition_result_t arming_state_transition(struct vehicle_status_s *current_state, const struct safety_s *safety,
arming_state_t new_arming_state, struct actuator_armed_s *armed, const int mavlink_fd = 0);
arming_state_t new_arming_state, struct actuator_armed_s *armed, const int mavlink_fd);
bool is_safe(const struct vehicle_status_s *current_state, const struct safety_s *safety, const struct actuator_armed_s *armed);

11
src/modules/fw_att_control/fw_att_control_main.cpp
View File

@ -707,14 +707,21 @@ FixedwingAttitudeControl::task_main()
float throttle_sp = 0.0f;
if (_vcontrol_mode.flag_control_velocity_enabled || _vcontrol_mode.flag_control_position_enabled) {
/* read in attitude setpoint from attitude setpoint uorb topic */
roll_sp = _att_sp.roll_body + _parameters.rollsp_offset_rad;
pitch_sp = _att_sp.pitch_body + _parameters.pitchsp_offset_rad;
throttle_sp = _att_sp.thrust;
/* reset integrals where needed */
if (_att_sp.roll_reset_integral)
if (_att_sp.roll_reset_integral) {
_roll_ctrl.reset_integrator();
}
if (_att_sp.pitch_reset_integral) {
_pitch_ctrl.reset_integrator();
}
if (_att_sp.yaw_reset_integral) {
_yaw_ctrl.reset_integrator();
}
} else {
/*
* Scale down roll and pitch as the setpoints are radians

14
src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp
View File

@ -841,6 +841,10 @@ FixedwingPositionControl::control_position(const math::Vector<2> &current_positi
/* current waypoint (the one currently heading for) */
math::Vector<2> curr_wp((float)pos_sp_triplet.current.lat, (float)pos_sp_triplet.current.lon);
/* Initialize attitude controller integrator reset flags to 0 */
_att_sp.roll_reset_integral = false;
_att_sp.pitch_reset_integral = false;
_att_sp.yaw_reset_integral = false;
/* previous waypoint */
math::Vector<2> prev_wp;
@ -1020,15 +1024,21 @@ FixedwingPositionControl::control_position(const math::Vector<2> &current_positi
} else if (pos_sp_triplet.current.type == SETPOINT_TYPE_TAKEOFF) {
/* Perform launch detection */
// warnx("Launch detection running");
if(!launch_detected) { //do not do further checks once a launch was detected
if (launchDetector.launchDetectionEnabled()) {
static hrt_abstime last_sent = 0;
if(hrt_absolute_time() - last_sent > 4e6) {
// warnx("Launch detection running");
mavlink_log_info(_mavlink_fd, "#audio: Launchdetection running");
last_sent = hrt_absolute_time();
}
/* Tell the attitude controller to stop integrating while we are waiting
* for the launch */
_att_sp.roll_reset_integral = true;
_att_sp.pitch_reset_integral = true;
_att_sp.yaw_reset_integral = true;
/* Detect launch */
launchDetector.update(_sensor_combined.accelerometer_m_s2[0]);
if (launchDetector.getLaunchDetected()) {
launch_detected = true;

14
src/modules/mavlink/mavlink_main.cpp
View File

@ -1555,13 +1555,18 @@ Mavlink::configure_stream(const char *stream_name, const float rate)
/* delete stream */
LL_DELETE(_streams, stream);
delete stream;
warnx("deleted stream %s", stream->get_name());
}
return OK;
}
}
if (interval > 0) {
if (interval == 0) {
/* stream was not active and is requested to be disabled, do nothing */
return OK;
}
/* search for stream with specified name in supported streams list */
for (unsigned int i = 0; streams_list[i] != nullptr; i++) {
@ -1572,14 +1577,13 @@ Mavlink::configure_stream(const char *stream_name, const float rate)
stream->set_interval(interval);
stream->subscribe(this);
LL_APPEND(_streams, stream);
return OK;
}
}
} else {
/* stream not found, nothing to disable */
return OK;
}
/* if we reach here, the stream list does not contain the stream */
warnx("stream %s not found", stream_name);
return ERROR;
}

10
src/modules/mavlink/mavlink_messages.cpp
View File

@ -226,7 +226,10 @@ protected:
struct vehicle_status_s status;
struct position_setpoint_triplet_s pos_sp_triplet;
if (status_sub->update(&status) && pos_sp_triplet_sub->update(&pos_sp_triplet)) {
/* always send the heartbeat, independent of the update status of the topics */
(void)status_sub->update(&status);
(void)pos_sp_triplet_sub->update(&pos_sp_triplet);
uint8_t mavlink_state = 0;
uint8_t mavlink_base_mode = 0;
uint32_t mavlink_custom_mode = 0;
@ -239,7 +242,6 @@ protected:
mavlink_custom_mode,
mavlink_state);
}
}
};
@ -1275,6 +1277,7 @@ protected:
// New message
mavlink_msg_rc_channels_send(_channel,
rc.timestamp_publication / 1000,
rc.channel_count,
((rc.channel_count > 0) ? rc.values[0] : UINT16_MAX),
((rc.channel_count > 1) ? rc.values[1] : UINT16_MAX),
((rc.channel_count > 2) ? rc.values[2] : UINT16_MAX),
@ -1293,7 +1296,6 @@ protected:
((rc.channel_count > 15) ? rc.values[15] : UINT16_MAX),
((rc.channel_count > 16) ? rc.values[16] : UINT16_MAX),
((rc.channel_count > 17) ? rc.values[17] : UINT16_MAX),
rc.channel_count,
rc.rssi);
}
}
@ -1625,7 +1627,7 @@ StreamListItem *streams_list[] = {
new StreamListItem(&MavlinkStreamLocalPositionSetpoint::new_instance, &MavlinkStreamLocalPositionSetpoint::get_name_static),
new StreamListItem(&MavlinkStreamRollPitchYawThrustSetpoint::new_instance, &MavlinkStreamRollPitchYawThrustSetpoint::get_name_static),
new StreamListItem(&MavlinkStreamRollPitchYawRatesThrustSetpoint::new_instance, &MavlinkStreamRollPitchYawRatesThrustSetpoint::get_name_static),
new StreamListItem(&MavlinkStreamRCChannelsRaw::new_instance, &MavlinkStreamGlobalPositionInt::get_name_static),
new StreamListItem(&MavlinkStreamRCChannelsRaw::new_instance, &MavlinkStreamRCChannelsRaw::get_name_static),
new StreamListItem(&MavlinkStreamManualControl::new_instance, &MavlinkStreamManualControl::get_name_static),
new StreamListItem(&MavlinkStreamOpticalFlow::new_instance, &MavlinkStreamOpticalFlow::get_name_static),
new StreamListItem(&MavlinkStreamAttitudeControls::new_instance, &MavlinkStreamAttitudeControls::get_name_static),

4
src/modules/systemlib/perf_counter.c
View File

@ -301,7 +301,7 @@ perf_print_counter_fd(int fd, perf_counter_t handle)
case PC_ELAPSED: {
struct perf_ctr_elapsed *pce = (struct perf_ctr_elapsed *)handle;
dprintf(fd, "%s: %llu events, %lluus elapsed, %llu avg, min %lluus max %lluus\n",
dprintf(fd, "%s: %llu events, %lluus elapsed, %lluus avg, min %lluus max %lluus\n",
handle->name,
pce->event_count,
pce->time_total,
@ -314,7 +314,7 @@ perf_print_counter_fd(int fd, perf_counter_t handle)
case PC_INTERVAL: {
struct perf_ctr_interval *pci = (struct perf_ctr_interval *)handle;
dprintf(fd, "%s: %llu events, %llu avg, min %lluus max %lluus\n",
dprintf(fd, "%s: %llu events, %lluus avg, min %lluus max %lluus\n",
handle->name,
pci->event_count,
(pci->time_last - pci->time_first) / pci->event_count,

2
src/modules/uORB/topics/vehicle_attitude_setpoint.h
View File

@ -72,6 +72,8 @@ struct vehicle_attitude_setpoint_s {
float thrust; /**< Thrust in Newton the power system should generate */
bool roll_reset_integral; /**< Reset roll integral part (navigation logic change) */
bool pitch_reset_integral; /**< Reset pitch integral part (navigation logic change) */
bool yaw_reset_integral; /**< Reset yaw integral part (navigation logic change) */
};