int uORBTest::UnitTest::test_unadvertise()
{
test_note("Testing unadvertise");
//we still have the advertisements from the previous test_multi calls.
for (int i = 0; i < 4; ++i) {
int ret = orb_unadvertise(_pfd[i]);
if (ret != PX4_OK) {
return test_fail("orb_unadvertise failed (%i)", ret);
}
}
//try to advertise and see whether we get the right instance
int instance_test[4];
struct orb_test t;
for (int i = 0; i < 4; ++i) {
_pfd[i] = orb_advertise_multi(ORB_ID(orb_multitest), &t, &instance_test[i], ORB_PRIO_MAX);
if (instance_test[i] != i) {
return test_fail("got wrong instance (should be %i, is %i)", i, instance_test[i]);
}
}
for (int i = 0; i < 4; ++i) {
orb_unadvertise(_pfd[i]);
}
return test_note("PASS unadvertise");
}
/**
* Creates a fake traffic measurement with supplied parameters.
*
*/
void Navigator::fake_traffic(const char *callsign, float distance, float direction, float traffic_heading,
float altitude_diff, float hor_velocity, float ver_velocity)
{
double lat, lon;
waypoint_from_heading_and_distance(get_global_position()->lat, get_global_position()->lon, direction, distance, &lat,
&lon);
float alt = get_global_position()->alt + altitude_diff;
// float vel_n = get_global_position()->vel_n;
// float vel_e = get_global_position()->vel_e;
// float vel_d = get_global_position()->vel_d;
transponder_report_s tr = {};
tr.timestamp = hrt_absolute_time();
tr.ICAO_address = 1234;
tr.lat = lat; // Latitude, expressed as degrees
tr.lon = lon; // Longitude, expressed as degrees
tr.altitude_type = 0;
tr.altitude = alt;
tr.heading = traffic_heading; //-atan2(vel_e, vel_n); // Course over ground in radians
tr.hor_velocity = hor_velocity; //sqrtf(vel_e * vel_e + vel_n * vel_n); // The horizontal velocity in m/s
tr.ver_velocity = ver_velocity; //-vel_d; // The vertical velocity in m/s, positive is up
strncpy(&tr.callsign[0], callsign, sizeof(tr.callsign));
tr.emitter_type = 0; // Type from ADSB_EMITTER_TYPE enum
tr.tslc = 2; // Time since last communication in seconds
tr.flags = transponder_report_s::PX4_ADSB_FLAGS_VALID_COORDS | transponder_report_s::PX4_ADSB_FLAGS_VALID_HEADING |
transponder_report_s::PX4_ADSB_FLAGS_VALID_VELOCITY |
transponder_report_s::PX4_ADSB_FLAGS_VALID_ALTITUDE |
transponder_report_s::PX4_ADSB_FLAGS_VALID_CALLSIGN; // Flags to indicate various statuses including valid data fields
tr.squawk = 6667;
orb_advert_t h = orb_advertise_queue(ORB_ID(transponder_report), &tr, transponder_report_s::ORB_QUEUE_LENGTH);
(void)orb_unadvertise(h);
}
MavlinkULog::~MavlinkULog()
{
if (_ulog_stream_ack_pub) {
orb_unadvertise(_ulog_stream_ack_pub);
}
if (_ulog_stream_sub >= 0) {
orb_unsubscribe(_ulog_stream_sub);
}
}
MavlinkParametersManager::~MavlinkParametersManager()
{
if (_uavcan_parameter_value_sub >= 0) {
orb_unsubscribe(_uavcan_parameter_value_sub);
}
if (_uavcan_parameter_request_pub) {
orb_unadvertise(_uavcan_parameter_request_pub);
}
}
void
CameraTrigger::test()
{
struct vehicle_command_s cmd = {};
cmd.command = vehicle_command_s::VEHICLE_CMD_DO_DIGICAM_CONTROL;
cmd.param5 = 1.0f;
orb_advert_t pub;
pub = orb_advertise_queue(ORB_ID(vehicle_command), &cmd, vehicle_command_s::ORB_QUEUE_LENGTH);
(void)orb_unadvertise(pub);
}
MPU9250::~MPU9250()
{
/* make sure we are truly inactive */
stop();
_call_interval = 0;
if (!_magnetometer_only) {
orb_unadvertise(_accel_topic);
orb_unadvertise(_gyro->_gyro_topic);
}
/* delete the accel subdriver */
delete _accel;
/* delete the gyro subdriver */
delete _gyro;
/* delete the magnetometer subdriver */
delete _mag;
/* free any existing reports */
if (_accel_reports != nullptr) {
delete _accel_reports;
}
if (_gyro_reports != nullptr) {
delete _gyro_reports;
}
/* delete the perf counter */
perf_free(_sample_perf);
perf_free(_accel_reads);
perf_free(_gyro_reads);
perf_free(_bad_transfers);
perf_free(_bad_registers);
perf_free(_good_transfers);
perf_free(_reset_retries);
perf_free(_duplicates);
}
OutputBase::~OutputBase()
{
if (_vehicle_attitude_sub >= 0) {
orb_unsubscribe(_vehicle_attitude_sub);
}
if (_vehicle_global_position_sub >= 0) {
orb_unsubscribe(_vehicle_global_position_sub);
}
if (_mount_orientation_pub) {
orb_unadvertise(_mount_orientation_pub);
}
}
int uORBTest::UnitTest::pub_test_multi2_main()
{
int data_next_idx = 0;
const int num_instances = 3;
orb_advert_t orb_pub[num_instances];
struct orb_test_medium data_topic;
for (int i = 0; i < num_instances; ++i) {
orb_advert_t &pub = orb_pub[i];
int idx = i;
// PX4_WARN("advertise %i, t=%" PRIu64, i, hrt_absolute_time());
pub = orb_advertise_multi(ORB_ID(orb_test_medium_multi), &data_topic, &idx, ORB_PRIO_DEFAULT);
if (idx != i) {
_thread_should_exit = true;
PX4_ERR("Got wrong instance! should be: %i, but is %i", i, idx);
return -1;
}
}
usleep(100 * 1000);
int message_counter = 0, num_messages = 50 * num_instances;
while (message_counter++ < num_messages) {
usleep(2); //make sure the timestamps are different
orb_advert_t &pub = orb_pub[data_next_idx];
data_topic.time = hrt_absolute_time();
data_topic.val = data_next_idx;
orb_publish(ORB_ID(orb_test_medium_multi), pub, &data_topic);
// PX4_WARN("publishing msg (idx=%i, t=%" PRIu64 ")", data_next_idx, data_topic.time);
data_next_idx = (data_next_idx + 1) % num_instances;
if (data_next_idx == 0) {
usleep(50 * 1000);
}
}
usleep(100 * 1000);
_thread_should_exit = true;
for (int i = 0; i < num_instances; ++i) {
orb_unadvertise(orb_pub[i]);
}
return 0;
}
MPU9250::~MPU9250()
{
/* make sure we are truly inactive */
stop();
orb_unadvertise(_accel_topic);
orb_unadvertise(_gyro->_gyro_topic);
/* delete the gyro subdriver */
delete _gyro;
/* delete the magnetometer subdriver */
delete _mag;
/* free any existing reports */
if (_accel_reports != nullptr) {
delete _accel_reports;
}
if (_gyro_reports != nullptr) {
delete _gyro_reports;
}
if (_accel_class_instance != -1) {
unregister_class_devname(ACCEL_BASE_DEVICE_PATH, _accel_class_instance);
}
/* delete the perf counter */
perf_free(_sample_perf);
perf_free(_accel_reads);
perf_free(_gyro_reads);
perf_free(_bad_transfers);
perf_free(_bad_registers);
perf_free(_good_transfers);
perf_free(_reset_retries);
perf_free(_duplicates);
}
void
CameraTrigger::test()
{
struct vehicle_command_s cmd = {
.timestamp = hrt_absolute_time(),
.param5 = 1.0f,
.param6 = 0.0f,
.param1 = 0.0f,
.param2 = 0.0f,
.param3 = 0.0f,
.param4 = 0.0f,
.param7 = 0.0f,
.command = vehicle_command_s::VEHICLE_CMD_DO_DIGICAM_CONTROL
};
orb_advert_t pub = orb_advertise_queue(ORB_ID(vehicle_command), &cmd, vehicle_command_s::ORB_QUEUE_LENGTH);
(void)orb_unadvertise(pub);
}
SF1XX::~SF1XX()
{
/* make sure we are truly inactive */
stop();
/* free any existing reports */
if (_reports != nullptr) {
delete _reports;
}
if (_distance_sensor_topic != nullptr) {
orb_unadvertise(_distance_sensor_topic);
}
if (_class_instance != -1) {
unregister_class_devname(RANGE_FINDER_BASE_DEVICE_PATH, _class_instance);
}
/* free perf counters */
perf_free(_sample_perf);
perf_free(_comms_errors);
}
leddar_one::~leddar_one()
{
stop();
free((char *)_serial_port);
if (_fd > -1) {
::close(_fd);
}
if (_reports) {
delete _reports;
}
if (_topic) {
orb_unadvertise(_topic);
}
perf_free(_sample_perf);
perf_free(_collect_timeout_perf);
perf_free(_comm_error);
}
LIS3MDL::~LIS3MDL()
{
/* make sure we are truly inactive */
stop();
if (_mag_topic != nullptr) {
orb_unadvertise(_mag_topic);
}
if (_reports != nullptr) {
delete _reports;
}
if (_class_instance != -1) {
unregister_class_devname(MAG_BASE_DEVICE_PATH, _class_instance);
}
// free perf counters
perf_free(_sample_perf);
perf_free(_comms_errors);
perf_free(_range_errors);
perf_free(_conf_errors);
}
int uORBTest::UnitTest::pub_test_queue_main()
{
struct orb_test_medium t;
orb_advert_t ptopic;
const unsigned int queue_size = 50;
t.val = 0;
if ((ptopic = orb_advertise_queue(ORB_ID(orb_test_medium_queue_poll), &t, queue_size)) == nullptr) {
_thread_should_exit = true;
return test_fail("advertise failed: %d", errno);
}
int message_counter = 0, num_messages = 20 * queue_size;
++t.val;
while (message_counter < num_messages) {
//simulate burst
int burst_counter = 0;
while (burst_counter++ < queue_size / 2 + 7) { //make interval non-boundary aligned
orb_publish(ORB_ID(orb_test_medium_queue_poll), ptopic, &t);
++t.val;
}
message_counter += burst_counter;
usleep(20 * 1000); //give subscriber a chance to catch up
}
_num_messages_sent = t.val;
usleep(100 * 1000);
_thread_should_exit = true;
orb_unadvertise(ptopic);
return 0;
}
OutputMavlink::~OutputMavlink()
{
if (_vehicle_command_pub) {
orb_unadvertise(_vehicle_command_pub);
}
}
int uORBTest::UnitTest::test_queue()
{
test_note("Testing orb queuing");
struct orb_test_medium t, u;
int sfd;
orb_advert_t ptopic;
bool updated;
sfd = orb_subscribe(ORB_ID(orb_test_medium_queue));
if (sfd < 0) {
return test_fail("subscribe failed: %d", errno);
}
const unsigned int queue_size = 11;
t.val = 0;
ptopic = orb_advertise_queue(ORB_ID(orb_test_medium_queue), &t, queue_size);
if (ptopic == nullptr) {
return test_fail("advertise failed: %d", errno);
}
orb_check(sfd, &updated);
if (!updated) {
return test_fail("update flag not set");
}
if (PX4_OK != orb_copy(ORB_ID(orb_test_medium_queue), sfd, &u)) {
return test_fail("copy(1) failed: %d", errno);
}
if (u.val != t.val) {
return test_fail("copy(1) mismatch: %d expected %d", u.val, t.val);
}
orb_check(sfd, &updated);
if (updated) {
return test_fail("spurious updated flag");
}
#define CHECK_UPDATED(element) \
orb_check(sfd, &updated); \
if (!updated) { \
return test_fail("update flag not set, element %i", element); \
}
#define CHECK_NOT_UPDATED(element) \
orb_check(sfd, &updated); \
if (updated) { \
return test_fail("update flag set, element %i", element); \
}
#define CHECK_COPY(i_got, i_correct) \
orb_copy(ORB_ID(orb_test_medium_queue), sfd, &u); \
if (i_got != i_correct) { \
return test_fail("got wrong element from the queue (got %i, should be %i)", i_got, i_correct); \
}
//no messages in the queue anymore
test_note(" Testing to write some elements...");
for (unsigned int i = 0; i < queue_size - 2; ++i) {
t.val = i;
orb_publish(ORB_ID(orb_test_medium_queue), ptopic, &t);
}
for (unsigned int i = 0; i < queue_size - 2; ++i) {
CHECK_UPDATED(i);
CHECK_COPY(u.val, i);
}
CHECK_NOT_UPDATED(queue_size);
test_note(" Testing overflow...");
int overflow_by = 3;
for (unsigned int i = 0; i < queue_size + overflow_by; ++i) {
t.val = i;
orb_publish(ORB_ID(orb_test_medium_queue), ptopic, &t);
}
for (unsigned int i = 0; i < queue_size; ++i) {
CHECK_UPDATED(i);
CHECK_COPY(u.val, i + overflow_by);
}
CHECK_NOT_UPDATED(queue_size);
test_note(" Testing underflow...");
for (unsigned int i = 0; i < queue_size; ++i) {
CHECK_NOT_UPDATED(i);
CHECK_COPY(u.val, queue_size + overflow_by - 1);
}
t.val = 943;
orb_publish(ORB_ID(orb_test_medium_queue), ptopic, &t);
CHECK_UPDATED(-1);
CHECK_COPY(u.val, t.val);
#undef CHECK_COPY
#undef CHECK_UPDATED
#undef CHECK_NOT_UPDATED
orb_unadvertise(ptopic);
return test_note("PASS orb queuing");
}
void *multirotor_attitude_control_thread_main()
{
/* welcome user */
fprintf (stdout, "Multirotor attitude controller started\n");
fflush(stdout);
int i;
bool_t updated, rates_sp_updated, reset_integral;
float rates[3];
/* store last control mode to detect mode switches */
bool_t control_yaw_position = 1 /* true */;
bool_t reset_yaw_sp = 1 /* true */;
/* declare and safely initialize all structs */
struct parameter_update_s update;
struct vehicle_attitude_s att;
memset(&att, 0, sizeof(att));
struct vehicle_attitude_setpoint_s att_sp;
memset(&att_sp, 0, sizeof(att_sp));
struct offboard_control_setpoint_s offboard_sp;
memset(&offboard_sp, 0, sizeof(offboard_sp));
struct vehicle_control_flags_s control_flags;
memset(&control_flags, 0, sizeof(control_flags));
struct manual_control_setpoint_s manual;
memset(&manual, 0, sizeof(manual));
struct sensor_combined_s sensor;
memset(&sensor, 0, sizeof(sensor));
struct vehicle_rates_setpoint_s rates_sp;
memset(&rates_sp, 0, sizeof(rates_sp));
struct vehicle_status_s status;
memset(&status, 0, sizeof(status));
struct actuator_controls_s actuators;
memset(&actuators, 0, sizeof(actuators));
/* subscribe */
orb_subscr_t vehicle_attitude_sub = orb_subscribe(ORB_ID(vehicle_attitude));
if (vehicle_attitude_sub < 0)
{
fprintf (stderr, "Attitude controller thread failed to subscribe to vehicle_attitude topic\n");
exit(-1);
}
orb_subscr_t parameter_update_sub = orb_subscribe(ORB_ID(parameter_update));
if (parameter_update_sub < 0)
{
fprintf (stderr, "Attitude controller thread failed to subscribe to parameter_update topic\n");
exit(-1);
}
orb_subscr_t vehicle_attitude_setpoint_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint));
if (vehicle_attitude_setpoint_sub < 0)
{
fprintf (stderr, "Attitude controller thread failed to subscribe to vehicle_attitude_setpoint topic\n");
exit(-1);
}
orb_subscr_t offboard_control_setpoint_sub = orb_subscribe(ORB_ID(offboard_control_setpoint));
if (offboard_control_setpoint_sub < 0)
{
fprintf (stderr, "Attitude controller thread failed to subscribe to offboard_control_setpoint topic\n");
exit(-1);
}
orb_subscr_t vehicle_control_flags_sub = orb_subscribe(ORB_ID(vehicle_control_flags));
if (vehicle_control_flags_sub < 0)
{
fprintf (stderr, "Attitude controller thread failed to subscribe to vehicle_control_flags topic\n");
exit(-1);
}
orb_subscr_t manual_control_setpoint_sub = orb_subscribe(ORB_ID(manual_control_setpoint));
if (manual_control_setpoint_sub < 0)
{
fprintf (stderr, "Attitude controller thread failed to subscribe to manual_control_setpoint topic\n");
exit(-1);
}
orb_subscr_t sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
if (sensor_combined_sub < 0)
{
fprintf (stderr, "Attitude controller thread failed to subscribe to sensor_combined topic\n");
exit(-1);
}
orb_subscr_t vehicle_rates_setpoint_sub = orb_subscribe(ORB_ID(vehicle_rates_setpoint));
if (vehicle_rates_setpoint_sub < 0)
{
fprintf (stderr, "Attitude controller thread failed to subscribe to vehicle_rates_setpoint topic\n");
exit(-1);
}
orb_subscr_t vehicle_status_sub = orb_subscribe(ORB_ID(vehicle_status));
if (vehicle_status_sub < 0)
{
fprintf (stderr, "Attitude controller thread failed to subscribe to vehicle_status topic\n");
exit(-1);
}
/* publish actuator controls */
for (i = 0; i < NUM_ACTUATOR_CONTROLS; i++) {
actuators.control[i] = 0.0f;
}
orb_advert_t actuator_pub = orb_advertise(ORB_ID_VEHICLE_ATTITUDE_CONTROLS);
if (actuator_pub == -1)
{
fprintf (stderr, "Comunicator thread failed to advertise the actutor_controls topic\n");
exit (-1);
}
orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators);
orb_advert_t att_sp_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint));
if (att_sp_pub == -1)
{
fprintf (stderr, "Comunicator thread failed to advertise the vehicle_attitude_setpoint topic\n");
exit (-1);
}
orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp);
orb_advert_t rates_sp_pub = orb_advertise(ORB_ID(vehicle_rates_setpoint));
if (rates_sp_pub == -1)
{
fprintf (stderr, "Comunicator thread failed to advertise the vehicle_rates_setpoint topic\n");
exit (-1);
}
orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp);
while (!_shutdown_all_systems) {
/* wait for a sensor update, check for exit condition every 500 ms */
updated = orb_poll(ORB_ID(vehicle_attitude), vehicle_attitude_sub, 500000);
/* timed out - periodic check for _shutdown_all_systems, etc. */
if (!updated)
continue;
/* this is undesirable but not much we can do - might want to flag unhappy status */
if (updated < 0) {
fprintf (stderr, "Attitude controller failed to poll vehicle attitude\n");
continue;
}
/* only run controller if attitude changed */
/* attitude */
orb_copy(ORB_ID(vehicle_attitude), vehicle_attitude_sub, &att);
/* parameters */
updated = orb_check (ORB_ID(parameter_update), parameter_update_sub);
if (updated) {
orb_copy(ORB_ID(parameter_update), parameter_update_sub, &update);
/* update parameters */
}
/* control mode */
updated = orb_check (ORB_ID(vehicle_control_flags), vehicle_control_flags_sub);
if (updated) {
orb_copy(ORB_ID(vehicle_control_flags), vehicle_control_flags_sub, &control_flags);
}
/* manual control setpoint */
updated = orb_check (ORB_ID(manual_control_setpoint), manual_control_setpoint_sub);
if (updated) {
orb_copy(ORB_ID(manual_control_setpoint), manual_control_setpoint_sub, &manual);
}
/* attitude setpoint */
updated = orb_check (ORB_ID(vehicle_attitude_setpoint), vehicle_attitude_setpoint_sub);
if (updated) {
orb_copy(ORB_ID(vehicle_attitude_setpoint), vehicle_attitude_setpoint_sub, &att_sp);
}
/* offboard control setpoint */
updated = orb_check (ORB_ID(offboard_control_setpoint), offboard_control_setpoint_sub);
if (updated) {
orb_copy(ORB_ID(offboard_control_setpoint), offboard_control_setpoint_sub, &offboard_sp);
}
/* vehicle status */
updated = orb_check (ORB_ID(vehicle_status), vehicle_status_sub);
if (updated) {
orb_copy(ORB_ID(vehicle_status), vehicle_status_sub, &status);
}
/* sensors */
updated = orb_check (ORB_ID(sensor_combined), sensor_combined_sub);
if (updated) {
orb_copy(ORB_ID(sensor_combined), sensor_combined_sub, &sensor);
}
/* set flag to safe value */
control_yaw_position = 1 /* true */;
/* reset yaw setpoint if not armed */
if (!control_flags.flag_armed) {
reset_yaw_sp = 1 /* true */;
}
/* define which input is the dominating control input */
if (control_flags.flag_control_offboard_enabled) {
/* offboard inputs */
if (offboard_sp.mode == OFFBOARD_CONTROL_MODE_DIRECT_RATES) {
rates_sp.roll = offboard_sp.p1;
rates_sp.pitch = offboard_sp.p2;
rates_sp.yaw = offboard_sp.p3;
rates_sp.thrust = offboard_sp.p4;
rates_sp.timestamp = get_absolute_time();
orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp);
} else if (offboard_sp.mode == OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE) {
att_sp.roll_body = offboard_sp.p1;
att_sp.pitch_body = offboard_sp.p2;
att_sp.yaw_body = offboard_sp.p3;
att_sp.thrust = offboard_sp.p4;
att_sp.timestamp = get_absolute_time();
/* publish the result to the vehicle actuators */
orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp);
}
/* reset yaw setpoint after offboard control */
reset_yaw_sp = 1 /* true */;
} else if (control_flags.flag_control_manual_enabled) {
/* manual input */
if (control_flags.flag_control_attitude_enabled) {
/* control attitude, update attitude setpoint depending on mode */
if (att_sp.thrust < 0.1f) {
/* no thrust, don't try to control yaw */
rates_sp.yaw = 0.0f;
control_yaw_position = 0 /* false */;
if (status.condition_landed) {
/* reset yaw setpoint if on ground */
reset_yaw_sp = 1 /* true */;
}
} else {
/* only move yaw setpoint if manual input is != 0 */
if (manual.yaw < -yaw_deadzone || yaw_deadzone < manual.yaw) {
/* control yaw rate */
control_yaw_position = 0 /* false */;
rates_sp.yaw = manual.yaw;
reset_yaw_sp = 1 /* true */; // has no effect on control, just for beautiful log
} else {
control_yaw_position = 1 /* true */;
}
}
if (!control_flags.flag_control_velocity_enabled) {
/* update attitude setpoint if not in position control mode */
att_sp.roll_body = manual.roll;
att_sp.pitch_body = manual.pitch;
if (!control_flags.flag_control_climb_rate_enabled) {
/* pass throttle directly if not in altitude control mode */
att_sp.thrust = manual.thrust;
}
}
/* reset yaw setpint to current position if needed */
if (reset_yaw_sp) {
att_sp.yaw_body = att.yaw;
reset_yaw_sp = 0 /* false */;
}
/*if (motor_test_mode) {
printf("testmode");
att_sp.roll_body = 0.0f;
att_sp.pitch_body = 0.0f;
att_sp.yaw_body = 0.0f;
att_sp.thrust = 0.1f;
}*/
att_sp.timestamp = get_absolute_time();
/* publish the attitude setpoint */
orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp);
} else {
/* manual rate inputs (ACRO), from RC control or joystick */
if (control_flags.flag_control_rates_enabled) {
rates_sp.roll = manual.roll;
rates_sp.pitch = manual.pitch;
rates_sp.yaw = manual.yaw;
rates_sp.thrust = manual.thrust;
rates_sp.timestamp = get_absolute_time();
}
/* reset yaw setpoint after ACRO */
reset_yaw_sp = 1 /* true */;
}
} else {
if (!control_flags.flag_control_auto_enabled) {
/* no control, try to stay on place */
if (!control_flags.flag_control_velocity_enabled) {
/* no velocity control, reset attitude setpoint */
att_sp.roll_body = 0.0f;
att_sp.pitch_body = 0.0f;
att_sp.timestamp = get_absolute_time();
orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp);
}
}
/* reset yaw setpoint after non-manual control */
reset_yaw_sp = 1 /* true */;
}
/* check if we should we reset integrals */
reset_integral = !control_flags.flag_armed || att_sp.thrust < 0.1f; // TODO use landed status instead of throttle
/* run attitude controller if needed */
if (control_flags.flag_control_attitude_enabled) {
multirotor_control_attitude(&att_sp, &att, &rates_sp, control_yaw_position, reset_integral);
orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp);
}
/* run rates controller if needed */
if (control_flags.flag_control_rates_enabled) {
/* get current rate setpoint */
rates_sp_updated = orb_check (ORB_ID(vehicle_rates_setpoint), vehicle_rates_setpoint_sub);
if (rates_sp_updated) {
orb_copy(ORB_ID(vehicle_rates_setpoint), vehicle_rates_setpoint_sub, &rates_sp);
}
/* apply controller */
rates[0] = att.roll_rate;
rates[1] = att.pitch_rate;
rates[2] = att.yaw_rate;
multirotor_control_rates(&rates_sp, rates, &actuators, reset_integral);
} else {
/* rates controller disabled, set actuators to zero for safety */
actuators.control[0] = 0.0f;
actuators.control[1] = 0.0f;
actuators.control[2] = 0.0f;
actuators.control[3] = 0.0f;
}
/* fill in manual control values */
actuators.control[4] = manual.flaps;
//actuators.control[5] = manual.aux1;
//actuators.control[6] = manual.aux2;
//actuators.control[7] = manual.aux3;
orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators);
}
fprintf (stdout, "INFO: Attitude controller exiting, disarming motors\n");
fflush (stdout);
/* kill all outputs */
for (i = 0; i < NUM_ACTUATOR_CONTROLS; i++)
actuators.control[i] = 0.0f;
orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators);
/*
* do unsubscriptions
*/
orb_unsubscribe(ORB_ID(vehicle_attitude), vehicle_attitude_sub, pthread_self());
orb_unsubscribe(ORB_ID(parameter_update), parameter_update_sub, pthread_self());
orb_unsubscribe(ORB_ID(vehicle_attitude_setpoint), vehicle_attitude_setpoint_sub, pthread_self());
orb_unsubscribe(ORB_ID(offboard_control_setpoint), offboard_control_setpoint_sub, pthread_self());
orb_unsubscribe(ORB_ID(vehicle_control_flags), vehicle_control_flags_sub, pthread_self());
orb_unsubscribe(ORB_ID(manual_control_setpoint), manual_control_setpoint_sub, pthread_self());
orb_unsubscribe(ORB_ID(sensor_combined), sensor_combined_sub, pthread_self());
orb_unsubscribe(ORB_ID(vehicle_rates_setpoint), vehicle_rates_setpoint_sub, pthread_self());
orb_unsubscribe(ORB_ID(vehicle_status), vehicle_status_sub, pthread_self());
/*
* do unadvertises
*/
orb_unadvertise(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, pthread_self());
orb_unadvertise(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, pthread_self());
orb_unadvertise(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, pthread_self());
return 0;
}
int uORBTest::UnitTest::test_single()
{
test_note("try single-topic support");
struct orb_test t, u;
int sfd;
orb_advert_t ptopic;
bool updated;
t.val = 0;
ptopic = orb_advertise(ORB_ID(orb_test), &t);
if (ptopic == nullptr) {
return test_fail("advertise failed: %d", errno);
}
test_note("publish handle 0x%08x", ptopic);
sfd = orb_subscribe(ORB_ID(orb_test));
if (sfd < 0) {
return test_fail("subscribe failed: %d", errno);
}
test_note("subscribe fd %d", sfd);
u.val = 1;
if (PX4_OK != orb_copy(ORB_ID(orb_test), sfd, &u)) {
return test_fail("copy(1) failed: %d", errno);
}
if (u.val != t.val) {
return test_fail("copy(1) mismatch: %d expected %d", u.val, t.val);
}
if (PX4_OK != orb_check(sfd, &updated)) {
return test_fail("check(1) failed");
}
if (updated) {
return test_fail("spurious updated flag");
}
t.val = 2;
test_note("try publish");
if (PX4_OK != orb_publish(ORB_ID(orb_test), ptopic, &t)) {
return test_fail("publish failed");
}
if (PX4_OK != orb_check(sfd, &updated)) {
return test_fail("check(2) failed");
}
if (!updated) {
return test_fail("missing updated flag");
}
if (PX4_OK != orb_copy(ORB_ID(orb_test), sfd, &u)) {
return test_fail("copy(2) failed: %d", errno);
}
if (u.val != t.val) {
return test_fail("copy(2) mismatch: %d expected %d", u.val, t.val);
}
orb_unsubscribe(sfd);
int ret = orb_unadvertise(ptopic);
if (ret != PX4_OK) {
return test_fail("orb_unadvertise failed: %i", ret);
}
return test_note("PASS single-topic test");
}
void
GPS::task_main()
{
/* open the serial port */
_serial_fd = ::open(_port, O_RDWR | O_NOCTTY);
if (_serial_fd < 0) {
PX4_ERR("GPS: failed to open serial port: %s err: %d", _port, errno);
/* tell the dtor that we are exiting, set error code */
_task = -1;
px4_task_exit(1);
}
#ifndef __PX4_QURT
// TODO: this call is not supported on Snapdragon just yet.
// However it seems to be nonblocking anyway and working.
int flags = fcntl(_serial_fd, F_GETFL, 0);
fcntl(_serial_fd, F_SETFL, flags | O_NONBLOCK);
#endif
for (int i = 0; i < _orb_inject_data_fd_count; ++i) {
_orb_inject_data_fd[i] = orb_subscribe_multi(ORB_ID(gps_inject_data), i);
}
initializeCommunicationDump();
uint64_t last_rate_measurement = hrt_absolute_time();
unsigned last_rate_count = 0;
/* loop handling received serial bytes and also configuring in between */
while (!_task_should_exit) {
if (_fake_gps) {
_report_gps_pos.timestamp = hrt_absolute_time();
_report_gps_pos.lat = (int32_t)47.378301e7f;
_report_gps_pos.lon = (int32_t)8.538777e7f;
_report_gps_pos.alt = (int32_t)1200e3f;
_report_gps_pos.s_variance_m_s = 10.0f;
_report_gps_pos.c_variance_rad = 0.1f;
_report_gps_pos.fix_type = 3;
_report_gps_pos.eph = 0.9f;
_report_gps_pos.epv = 1.8f;
_report_gps_pos.vel_n_m_s = 0.0f;
_report_gps_pos.vel_e_m_s = 0.0f;
_report_gps_pos.vel_d_m_s = 0.0f;
_report_gps_pos.vel_m_s = sqrtf(_report_gps_pos.vel_n_m_s * _report_gps_pos.vel_n_m_s + _report_gps_pos.vel_e_m_s *
_report_gps_pos.vel_e_m_s + _report_gps_pos.vel_d_m_s * _report_gps_pos.vel_d_m_s);
_report_gps_pos.cog_rad = 0.0f;
_report_gps_pos.vel_ned_valid = true;
/* no time and satellite information simulated */
publish();
usleep(2e5);
} else {
if (_helper != nullptr) {
delete(_helper);
/* set to zero to ensure parser is not used while not instantiated */
_helper = nullptr;
}
switch (_mode) {
case GPS_DRIVER_MODE_UBX:
_helper = new GPSDriverUBX(&GPS::callback, this, &_report_gps_pos, _p_report_sat_info);
break;
case GPS_DRIVER_MODE_MTK:
_helper = new GPSDriverMTK(&GPS::callback, this, &_report_gps_pos);
break;
case GPS_DRIVER_MODE_ASHTECH:
_helper = new GPSDriverAshtech(&GPS::callback, this, &_report_gps_pos, _p_report_sat_info);
break;
default:
break;
}
/* the Ashtech driver lies about successful configuration and the
* MTK driver is not well tested, so we really only trust the UBX
* driver for an advance publication
*/
if (_helper->configure(_baudrate, GPSHelper::OutputMode::GPS) == 0) {
/* reset report */
memset(&_report_gps_pos, 0, sizeof(_report_gps_pos));
if (_mode == GPS_DRIVER_MODE_UBX) {
/* Publish initial report that we have access to a GPS,
* but set all critical state fields to indicate we have
* no valid position lock
*/
/* reset the timestamp for data, because we have no data yet */
_report_gps_pos.timestamp = 0;
_report_gps_pos.timestamp_time_relative = 0;
/* set a massive variance */
_report_gps_pos.eph = 10000.0f;
_report_gps_pos.epv = 10000.0f;
_report_gps_pos.fix_type = 0;
publish();
/* GPS is obviously detected successfully, reset statistics */
_helper->resetUpdateRates();
}
int helper_ret;
while ((helper_ret = _helper->receive(TIMEOUT_5HZ)) > 0 && !_task_should_exit) {
if (helper_ret & 1) {
publish();
last_rate_count++;
}
if (_p_report_sat_info && (helper_ret & 2)) {
publishSatelliteInfo();
}
/* measure update rate every 5 seconds */
if (hrt_absolute_time() - last_rate_measurement > RATE_MEASUREMENT_PERIOD) {
float dt = (float)((hrt_absolute_time() - last_rate_measurement)) / 1000000.0f;
_rate = last_rate_count / dt;
_rate_rtcm_injection = _last_rate_rtcm_injection_count / dt;
last_rate_measurement = hrt_absolute_time();
last_rate_count = 0;
_last_rate_rtcm_injection_count = 0;
_helper->storeUpdateRates();
_helper->resetUpdateRates();
}
if (!_healthy) {
// Helpful for debugging, but too verbose for normal ops
// const char *mode_str = "unknown";
//
// switch (_mode) {
// case GPS_DRIVER_MODE_UBX:
// mode_str = "UBX";
// break;
//
// case GPS_DRIVER_MODE_MTK:
// mode_str = "MTK";
// break;
//
// case GPS_DRIVER_MODE_ASHTECH:
// mode_str = "ASHTECH";
// break;
//
// default:
// break;
// }
//
// PX4_WARN("module found: %s", mode_str);
_healthy = true;
}
//check for disarming
if (_vehicle_status_sub != -1 && _dump_from_gps_device_fd != -1) {
bool updated;
orb_check(_vehicle_status_sub, &updated);
if (updated) {
vehicle_status_s vehicle_status;
orb_copy(ORB_ID(vehicle_status), _vehicle_status_sub, &vehicle_status);
bool armed = (vehicle_status.arming_state == vehicle_status_s::ARMING_STATE_ARMED) ||
(vehicle_status.arming_state == vehicle_status_s::ARMING_STATE_ARMED_ERROR);
if (armed) {
_is_armed = true;
} else if (_is_armed) {
//disable communication dump when disarming
close(_dump_from_gps_device_fd);
_dump_from_gps_device_fd = -1;
close(_dump_to_gps_device_fd);
_dump_to_gps_device_fd = -1;
_is_armed = false;
}
}
}
}
if (_healthy) {
PX4_WARN("GPS module lost");
_healthy = false;
_rate = 0.0f;
_rate_rtcm_injection = 0.0f;
}
}
/* select next mode */
switch (_mode) {
case GPS_DRIVER_MODE_UBX:
_mode = GPS_DRIVER_MODE_MTK;
break;
case GPS_DRIVER_MODE_MTK:
_mode = GPS_DRIVER_MODE_ASHTECH;
break;
case GPS_DRIVER_MODE_ASHTECH:
_mode = GPS_DRIVER_MODE_UBX;
break;
default:
break;
}
}
}
PX4_WARN("exiting");
for (size_t i = 0; i < _orb_inject_data_fd_count; ++i) {
orb_unsubscribe(_orb_inject_data_fd[i]);
_orb_inject_data_fd[i] = -1;
}
if (_dump_to_gps_device_fd != -1) {
close(_dump_to_gps_device_fd);
_dump_to_gps_device_fd = -1;
}
if (_dump_from_gps_device_fd != -1) {
close(_dump_from_gps_device_fd);
_dump_from_gps_device_fd = -1;
}
if (_vehicle_status_sub != -1) {
orb_unsubscribe(_vehicle_status_sub);
_vehicle_status_sub = -1;
}
::close(_serial_fd);
orb_unadvertise(_report_gps_pos_pub);
/* tell the dtor that we are exiting */
_task = -1;
px4_task_exit(0);
}
/**
* Mission waypoint manager main function
*/
void *mission_waypoint_manager_thread_main(void* args)
{
absolute_time now;
int updated;
float turn_distance;
/* initialize waypoint manager */
// ************************************* subscribe ******************************************
global_position_setpoint_pub = orb_advertise (ORB_ID(vehicle_global_position_setpoint));
if (global_position_setpoint_pub == -1)
{
fprintf (stderr, "Waypoint manager thread failed to advertise the vehicle_global_position_setpoint topic\n");
exit (-1);
}
global_position_set_triplet_pub = orb_advertise (ORB_ID(vehicle_global_position_set_triplet));
if (global_position_set_triplet_pub == -1)
{
fprintf (stderr, "Waypoint manager thread failed to advertise the vehicle_global_position_set_triplet topic\n");
exit (-1);
}
// ************************************* subscribe ******************************************
struct vehicle_global_position_s global_pos;
orb_subscr_t global_pos_sub = orb_subscribe (ORB_ID(vehicle_global_position));
if (global_pos_sub == -1)
{
fprintf (stderr, "Waypoint manager thread failed to subscribe the vehicle_global_position topic\n");
exit (-1);
}
struct vehicle_control_flags_s control_flags;
orb_subscr_t control_flags_sub = orb_subscribe(ORB_ID(vehicle_control_flags));
if (control_flags_sub < 0)
{
fprintf (stderr, "Waypoint manager thread failed to subscribe to vehicle_control_flags topic\n");
exit(-1);
}
struct navigation_capabilities_s nav_cap;
orb_subscr_t nav_cap_sub = orb_subscribe (ORB_ID(navigation_capabilities));
if (nav_cap_sub == -1)
{
fprintf (stderr, "Waypoint manager thread failed to subscribe the navigation_capabilities topic\n");
exit (-1);
}
struct parameter_update_s params;
orb_subscr_t param_sub = orb_subscribe (ORB_ID(parameter_update));
if (param_sub == -1)
{
fprintf (stderr, "Waypoint manager thread failed to subscribe the parameter_update topic\n");
exit (-1);
}
orb_subscr_t mission_sub = orb_subscribe (ORB_ID(mission));
if (mission_sub == -1)
{
fprintf (stderr, "Waypoint manager thread failed to subscribe the mission topic\n");
exit (-1);
}
orb_subscr_t home_sub = orb_subscribe (ORB_ID(home_position));
if (home_sub == -1)
{
fprintf (stderr, "Waypoint manager thread failed to subscribe the home_position topic\n");
exit (-1);
}
/* abort on a nonzero return value from the parameter init */
if (mission_waypoint_manager_params_init() != 0 || wp_manager_init (mission_sub, home_sub) != 0)
{
fprintf (stderr, "Waypoint manager exiting on startup due to an error\n");
exit (-1);
}
turn_distance = (is_rotary_wing)? mission_waypoint_manager_parameters.mr_turn_distance :
mission_waypoint_manager_parameters.fw_turn_distance;
/* welcome user */
fprintf (stdout, "Waypoint manager started\n");
fflush(stdout);
/* waypoint main eventloop */
while (!_shutdown_all_systems) {
// wait for the position estimation for a max of 500ms
updated = orb_poll (ORB_ID(vehicle_global_position), global_pos_sub, 500000);
if (updated < 0)
{
// that's undesiderable but there is not much we can do
fprintf (stderr, "Waypoint manager thread experienced an error waiting for actuator_controls topic\n");
continue;
}
else if (updated == 0)
{
continue;
}
else
orb_copy (ORB_ID(vehicle_global_position), global_pos_sub, (void *) &global_pos);
updated = orb_check (ORB_ID(vehicle_control_flags), control_flags_sub);
if (updated) {
orb_copy(ORB_ID(vehicle_control_flags), control_flags_sub, &control_flags);
}
updated = orb_check (ORB_ID(navigation_capabilities), nav_cap_sub);
if (updated)
{
orb_copy (ORB_ID(navigation_capabilities), nav_cap_sub, (void *) &nav_cap);
turn_distance = (nav_cap.turn_distance > 0)? nav_cap.turn_distance : turn_distance;
}
updated = orb_check (ORB_ID(parameter_update), param_sub);
if (updated) {
/* clear updated flag */
orb_copy(ORB_ID(parameter_update), param_sub, ¶ms);
/* update multirotor_position_control_parameters */
mission_waypoint_manager_params_update();
}
if (!control_flags.flag_control_manual_enabled && control_flags.flag_control_auto_enabled)
{
orb_publish(ORB_ID(vehicle_global_position_setpoint), global_position_setpoint_pub, &g_sp);
orb_publish(ORB_ID(vehicle_global_position_set_triplet), global_position_set_triplet_pub, &triplet);
}
now = get_absolute_time();
/* check if waypoint has been reached against the last positions */
check_waypoints_reached(now, &global_pos, turn_distance);
/* sleep 25 ms */
usleep(25000);
}
/*
* do unsubscriptions
*/
if (orb_unsubscribe (ORB_ID(vehicle_global_position), global_pos_sub, pthread_self()) < 0)
fprintf (stderr, "Waypoint manager thread failed to unsubscribe to vehicle_global_position topic\n");
if (orb_unsubscribe(ORB_ID(vehicle_control_flags), control_flags_sub, pthread_self()) < 0)
fprintf (stderr, "Waypoint manager thread failed to unsubscribe to vehicle_control_flags topic\n");
if (orb_unsubscribe (ORB_ID(navigation_capabilities), nav_cap_sub, pthread_self()) < 0)
fprintf (stderr, "Waypoint manager thread failed to unsubscribe to navigation_capabilities topic\n");
if (orb_unsubscribe (ORB_ID(parameter_update), param_sub, pthread_self()) < 0)
fprintf (stderr, "Waypoint manager thread failed to unsubscribe to parameter_update topic\n");
if (orb_unsubscribe (ORB_ID(mission), mission_sub, pthread_self()) < 0)
fprintf (stderr, "Waypoint manager thread failed to unsubscribe to mission topic\n");
if (orb_unsubscribe (ORB_ID(home_position), home_sub, pthread_self()) < 0)
fprintf (stderr, "Waypoint manager thread failed to unsubscribe to home_position topic\n");
/*
* do unadvertises
*/
if (orb_unadvertise (ORB_ID(vehicle_global_position_setpoint), global_position_setpoint_pub, pthread_self()) < 0)
fprintf (stderr, "Waypoint manager thread failed to unadvertise the global_position_setpoint_pub topic\n");
if (orb_unadvertise (ORB_ID(vehicle_global_position_set_triplet), global_position_set_triplet_pub, pthread_self()) < 0)
fprintf (stderr, "Waypoint manager thread failed to unadvertise the vehicle_global_position_set_triplet topic\n");
return 0;
}
void
GPS::task_main()
{
/* open the serial port */
_serial_fd = ::open(_port, O_RDWR | O_NOCTTY);
if (_serial_fd < 0) {
PX4_ERR("GPS: failed to open serial port: %s err: %d", _port, errno);
/* tell the dtor that we are exiting, set error code */
_task = -1;
px4_task_exit(1);
}
_orb_inject_data_fd = orb_subscribe(ORB_ID(gps_inject_data));
initializeCommunicationDump();
uint64_t last_rate_measurement = hrt_absolute_time();
unsigned last_rate_count = 0;
/* loop handling received serial bytes and also configuring in between */
while (!_task_should_exit) {
if (_fake_gps) {
_report_gps_pos.timestamp = hrt_absolute_time();
_report_gps_pos.lat = (int32_t)47.378301e7f;
_report_gps_pos.lon = (int32_t)8.538777e7f;
_report_gps_pos.alt = (int32_t)1200e3f;
_report_gps_pos.alt_ellipsoid = 10000;
_report_gps_pos.s_variance_m_s = 0.5f;
_report_gps_pos.c_variance_rad = 0.1f;
_report_gps_pos.fix_type = 3;
_report_gps_pos.eph = 0.8f;
_report_gps_pos.epv = 1.2f;
_report_gps_pos.hdop = 0.9f;
_report_gps_pos.vdop = 0.9f;
_report_gps_pos.vel_n_m_s = 0.0f;
_report_gps_pos.vel_e_m_s = 0.0f;
_report_gps_pos.vel_d_m_s = 0.0f;
_report_gps_pos.vel_m_s = sqrtf(_report_gps_pos.vel_n_m_s * _report_gps_pos.vel_n_m_s + _report_gps_pos.vel_e_m_s *
_report_gps_pos.vel_e_m_s + _report_gps_pos.vel_d_m_s * _report_gps_pos.vel_d_m_s);
_report_gps_pos.cog_rad = 0.0f;
_report_gps_pos.vel_ned_valid = true;
_report_gps_pos.satellites_used = 10;
/* no time and satellite information simulated */
publish();
usleep(2e5);
} else {
if (_helper != nullptr) {
delete(_helper);
/* set to zero to ensure parser is not used while not instantiated */
_helper = nullptr;
}
switch (_mode) {
case GPS_DRIVER_MODE_NONE:
_mode = GPS_DRIVER_MODE_UBX;
//no break
case GPS_DRIVER_MODE_UBX:
_helper = new GPSDriverUBX(_interface, &GPS::callback, this, &_report_gps_pos, _p_report_sat_info);
break;
case GPS_DRIVER_MODE_MTK:
_helper = new GPSDriverMTK(&GPS::callback, this, &_report_gps_pos);
break;
case GPS_DRIVER_MODE_ASHTECH:
_helper = new GPSDriverAshtech(&GPS::callback, this, &_report_gps_pos, _p_report_sat_info);
break;
default:
break;
}
/* the Ashtech driver lies about successful configuration and the
* MTK driver is not well tested, so we really only trust the UBX
* driver for an advance publication
*/
if (_helper->configure(_baudrate, GPSHelper::OutputMode::GPS) == 0) {
/* reset report */
memset(&_report_gps_pos, 0, sizeof(_report_gps_pos));
if (_mode == GPS_DRIVER_MODE_UBX) {
/* Publish initial report that we have access to a GPS,
* but set all critical state fields to indicate we have
* no valid position lock
*/
/* reset the timestamp for data, because we have no data yet */
_report_gps_pos.timestamp = 0;
_report_gps_pos.timestamp_time_relative = 0;
/* set a massive variance */
_report_gps_pos.eph = 10000.0f;
_report_gps_pos.epv = 10000.0f;
_report_gps_pos.fix_type = 0;
publish();
/* GPS is obviously detected successfully, reset statistics */
_helper->resetUpdateRates();
}
int helper_ret;
while ((helper_ret = _helper->receive(TIMEOUT_5HZ)) > 0 && !_task_should_exit) {
if (helper_ret & 1) {
publish();
last_rate_count++;
}
if (_p_report_sat_info && (helper_ret & 2)) {
publishSatelliteInfo();
}
/* measure update rate every 5 seconds */
if (hrt_absolute_time() - last_rate_measurement > RATE_MEASUREMENT_PERIOD) {
float dt = (float)((hrt_absolute_time() - last_rate_measurement)) / 1000000.0f;
_rate = last_rate_count / dt;
_rate_rtcm_injection = _last_rate_rtcm_injection_count / dt;
last_rate_measurement = hrt_absolute_time();
last_rate_count = 0;
_last_rate_rtcm_injection_count = 0;
_helper->storeUpdateRates();
_helper->resetUpdateRates();
}
if (!_healthy) {
// Helpful for debugging, but too verbose for normal ops
// const char *mode_str = "unknown";
//
// switch (_mode) {
// case GPS_DRIVER_MODE_UBX:
// mode_str = "UBX";
// break;
//
// case GPS_DRIVER_MODE_MTK:
// mode_str = "MTK";
// break;
//
// case GPS_DRIVER_MODE_ASHTECH:
// mode_str = "ASHTECH";
// break;
//
// default:
// break;
// }
//
// PX4_WARN("module found: %s", mode_str);
_healthy = true;
}
}
if (_healthy) {
PX4_WARN("GPS module lost");
_healthy = false;
_rate = 0.0f;
_rate_rtcm_injection = 0.0f;
}
}
if (_mode_auto) {
switch (_mode) {
case GPS_DRIVER_MODE_UBX:
_mode = GPS_DRIVER_MODE_MTK;
break;
case GPS_DRIVER_MODE_MTK:
_mode = GPS_DRIVER_MODE_ASHTECH;
break;
case GPS_DRIVER_MODE_ASHTECH:
_mode = GPS_DRIVER_MODE_UBX;
break;
default:
break;
}
}
}
}
PX4_INFO("exiting");
orb_unsubscribe(_orb_inject_data_fd);
if (_dump_communication_pub) {
orb_unadvertise(_dump_communication_pub);
}
::close(_serial_fd);
orb_unadvertise(_report_gps_pos_pub);
/* tell the dtor that we are exiting */
_task = -1;
px4_task_exit(0);
}
PublicationBase::~PublicationBase()
{
orb_unadvertise(getHandle());
}
void
Navigator::task_main()
{
bool have_geofence_position_data = false;
/* Try to load the geofence:
* if /fs/microsd/etc/geofence.txt load from this file
* else clear geofence data in datamanager */
struct stat buffer;
if (stat(GEOFENCE_FILENAME, &buffer) == 0) {
PX4_INFO("Try to load geofence.txt");
_geofence.loadFromFile(GEOFENCE_FILENAME);
} else {
if (_geofence.clearDm() != OK) {
mavlink_log_critical(&_mavlink_log_pub, "failed clearing geofence");
}
}
/* do subscriptions */
_global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
_local_pos_sub = orb_subscribe(ORB_ID(vehicle_local_position));
_gps_pos_sub = orb_subscribe(ORB_ID(vehicle_gps_position));
_sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
_fw_pos_ctrl_status_sub = orb_subscribe(ORB_ID(fw_pos_ctrl_status));
_vstatus_sub = orb_subscribe(ORB_ID(vehicle_status));
_land_detected_sub = orb_subscribe(ORB_ID(vehicle_land_detected));
_home_pos_sub = orb_subscribe(ORB_ID(home_position));
_onboard_mission_sub = orb_subscribe(ORB_ID(onboard_mission));
_offboard_mission_sub = orb_subscribe(ORB_ID(offboard_mission));
_param_update_sub = orb_subscribe(ORB_ID(parameter_update));
_vehicle_command_sub = orb_subscribe(ORB_ID(vehicle_command));
/* copy all topics first time */
vehicle_status_update();
vehicle_land_detected_update();
global_position_update();
local_position_update();
gps_position_update();
sensor_combined_update();
home_position_update(true);
fw_pos_ctrl_status_update();
params_update();
/* wakeup source(s) */
px4_pollfd_struct_t fds[1] = {};
/* Setup of loop */
fds[0].fd = _global_pos_sub;
fds[0].events = POLLIN;
bool global_pos_available_once = false;
/* rate-limit global pos subscription to 20 Hz / 50 ms */
orb_set_interval(_global_pos_sub, 49);
while (!_task_should_exit) {
/* wait for up to 1000ms for data */
int pret = px4_poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 1000);
if (pret == 0) {
/* timed out - periodic check for _task_should_exit, etc. */
if (global_pos_available_once) {
global_pos_available_once = false;
PX4_WARN("global position timeout");
}
/* Let the loop run anyway, don't do `continue` here. */
} else if (pret < 0) {
/* this is undesirable but not much we can do - might want to flag unhappy status */
PX4_ERR("nav: poll error %d, %d", pret, errno);
usleep(10000);
continue;
} else {
if (fds[0].revents & POLLIN) {
/* success, global pos is available */
global_position_update();
if (_geofence.getSource() == Geofence::GF_SOURCE_GLOBALPOS) {
have_geofence_position_data = true;
}
global_pos_available_once = true;
}
}
perf_begin(_loop_perf);
bool updated;
/* gps updated */
orb_check(_gps_pos_sub, &updated);
if (updated) {
gps_position_update();
if (_geofence.getSource() == Geofence::GF_SOURCE_GPS) {
have_geofence_position_data = true;
}
}
/* local position updated */
orb_check(_local_pos_sub, &updated);
if (updated) {
local_position_update();
}
/* sensors combined updated */
orb_check(_sensor_combined_sub, &updated);
if (updated) {
sensor_combined_update();
}
/* parameters updated */
orb_check(_param_update_sub, &updated);
if (updated) {
params_update();
}
/* vehicle status updated */
orb_check(_vstatus_sub, &updated);
if (updated) {
vehicle_status_update();
}
/* vehicle land detected updated */
orb_check(_land_detected_sub, &updated);
if (updated) {
vehicle_land_detected_update();
}
/* navigation capabilities updated */
orb_check(_fw_pos_ctrl_status_sub, &updated);
if (updated) {
fw_pos_ctrl_status_update();
}
/* home position updated */
orb_check(_home_pos_sub, &updated);
if (updated) {
home_position_update();
}
orb_check(_vehicle_command_sub, &updated);
if (updated) {
vehicle_command_s cmd = {};
orb_copy(ORB_ID(vehicle_command), _vehicle_command_sub, &cmd);
if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_REPOSITION) {
struct position_setpoint_triplet_s *rep = get_reposition_triplet();
// store current position as previous position and goal as next
rep->previous.yaw = get_global_position()->yaw;
rep->previous.lat = get_global_position()->lat;
rep->previous.lon = get_global_position()->lon;
rep->previous.alt = get_global_position()->alt;
rep->current.loiter_radius = get_loiter_radius();
rep->current.loiter_direction = 1;
rep->current.type = position_setpoint_s::SETPOINT_TYPE_LOITER;
// Go on and check which changes had been requested
if (PX4_ISFINITE(cmd.param4)) {
rep->current.yaw = cmd.param4;
} else {
rep->current.yaw = NAN;
}
if (PX4_ISFINITE(cmd.param5) && PX4_ISFINITE(cmd.param6)) {
rep->current.lat = (cmd.param5 < 1000) ? cmd.param5 : cmd.param5 / (double)1e7;
rep->current.lon = (cmd.param6 < 1000) ? cmd.param6 : cmd.param6 / (double)1e7;
} else {
rep->current.lat = get_global_position()->lat;
rep->current.lon = get_global_position()->lon;
}
if (PX4_ISFINITE(cmd.param7)) {
rep->current.alt = cmd.param7;
} else {
rep->current.alt = get_global_position()->alt;
}
rep->previous.valid = true;
rep->current.valid = true;
rep->next.valid = false;
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_NAV_TAKEOFF) {
struct position_setpoint_triplet_s *rep = get_takeoff_triplet();
// store current position as previous position and goal as next
rep->previous.yaw = get_global_position()->yaw;
rep->previous.lat = get_global_position()->lat;
rep->previous.lon = get_global_position()->lon;
rep->previous.alt = get_global_position()->alt;
rep->current.loiter_radius = get_loiter_radius();
rep->current.loiter_direction = 1;
rep->current.type = position_setpoint_s::SETPOINT_TYPE_TAKEOFF;
if (home_position_valid()) {
rep->current.yaw = cmd.param4;
rep->previous.valid = true;
} else {
rep->current.yaw = get_local_position()->yaw;
rep->previous.valid = false;
}
if (PX4_ISFINITE(cmd.param5) && PX4_ISFINITE(cmd.param6)) {
rep->current.lat = (cmd.param5 < 1000) ? cmd.param5 : cmd.param5 / (double)1e7;
rep->current.lon = (cmd.param6 < 1000) ? cmd.param6 : cmd.param6 / (double)1e7;
} else {
// If one of them is non-finite, reset both
rep->current.lat = NAN;
rep->current.lon = NAN;
}
rep->current.alt = cmd.param7;
rep->current.valid = true;
rep->next.valid = false;
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_LAND_START) {
/* find NAV_CMD_DO_LAND_START in the mission and
* use MAV_CMD_MISSION_START to start the mission there
*/
int land_start = _mission.find_offboard_land_start();
if (land_start != -1) {
vehicle_command_s vcmd = {};
vcmd.target_system = get_vstatus()->system_id;
vcmd.target_component = get_vstatus()->component_id;
vcmd.command = vehicle_command_s::VEHICLE_CMD_MISSION_START;
vcmd.param1 = land_start;
vcmd.param2 = 0;
publish_vehicle_cmd(vcmd);
} else {
PX4_WARN("planned landing not available");
}
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_NAV_RETURN_TO_LAUNCH) {
vehicle_command_s vcmd = {};
vcmd.target_system = get_vstatus()->system_id;
vcmd.target_component = get_vstatus()->component_id;
vcmd.command = vehicle_command_s::VEHICLE_CMD_NAV_RETURN_TO_LAUNCH;
orb_advert_t pub = orb_advertise_queue(ORB_ID(vehicle_command), &vcmd, vehicle_command_s::ORB_QUEUE_LENGTH);
(void)orb_unadvertise(pub);
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_MISSION_START) {
if (get_mission_result()->valid &&
PX4_ISFINITE(cmd.param1) && (cmd.param1 >= 0) && (cmd.param1 < _mission_result.seq_total)) {
_mission.set_current_offboard_mission_index(cmd.param1);
}
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_PAUSE_CONTINUE) {
warnx("navigator: got pause/continue command");
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_CHANGE_SPEED) {
if (cmd.param2 > FLT_EPSILON) {
// XXX not differentiating ground and airspeed yet
set_cruising_speed(cmd.param2);
} else {
set_cruising_speed();
/* if no speed target was given try to set throttle */
if (cmd.param3 > FLT_EPSILON) {
set_cruising_throttle(cmd.param3 / 100);
} else {
set_cruising_throttle();
}
}
}
}
/* Check geofence violation */
static hrt_abstime last_geofence_check = 0;
if (have_geofence_position_data &&
(_geofence.getGeofenceAction() != geofence_result_s::GF_ACTION_NONE) &&
(hrt_elapsed_time(&last_geofence_check) > GEOFENCE_CHECK_INTERVAL)) {
bool inside = _geofence.inside(_global_pos, _gps_pos, _sensor_combined.baro_alt_meter, _home_pos,
home_position_valid());
last_geofence_check = hrt_absolute_time();
have_geofence_position_data = false;
_geofence_result.timestamp = hrt_absolute_time();
_geofence_result.geofence_action = _geofence.getGeofenceAction();
if (!inside) {
/* inform other apps via the mission result */
_geofence_result.geofence_violated = true;
/* Issue a warning about the geofence violation once */
if (!_geofence_violation_warning_sent) {
mavlink_log_critical(&_mavlink_log_pub, "Geofence violation");
_geofence_violation_warning_sent = true;
}
} else {
/* inform other apps via the mission result */
_geofence_result.geofence_violated = false;
/* Reset the _geofence_violation_warning_sent field */
_geofence_violation_warning_sent = false;
}
publish_geofence_result();
}
/* Do stuff according to navigation state set by commander */
switch (_vstatus.nav_state) {
case vehicle_status_s::NAVIGATION_STATE_AUTO_MISSION:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_mission;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LOITER:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_loiter;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RCRECOVER:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_rcLoss;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RTL:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_rtl;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_TAKEOFF:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_takeoff;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LAND:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_land;
break;
case vehicle_status_s::NAVIGATION_STATE_DESCEND:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_land;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RTGS:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_dataLinkLoss;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LANDENGFAIL:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_engineFailure;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LANDGPSFAIL:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_gpsFailure;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_FOLLOW_TARGET:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_follow_target;
break;
case vehicle_status_s::NAVIGATION_STATE_MANUAL:
case vehicle_status_s::NAVIGATION_STATE_ACRO:
case vehicle_status_s::NAVIGATION_STATE_ALTCTL:
case vehicle_status_s::NAVIGATION_STATE_POSCTL:
case vehicle_status_s::NAVIGATION_STATE_TERMINATION:
case vehicle_status_s::NAVIGATION_STATE_OFFBOARD:
case vehicle_status_s::NAVIGATION_STATE_STAB:
default:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = nullptr;
_can_loiter_at_sp = false;
break;
}
/* iterate through navigation modes and set active/inactive for each */
for (unsigned int i = 0; i < NAVIGATOR_MODE_ARRAY_SIZE; i++) {
_navigation_mode_array[i]->run(_navigation_mode == _navigation_mode_array[i]);
}
/* if nothing is running, set position setpoint triplet invalid once */
if (_navigation_mode == nullptr && !_pos_sp_triplet_published_invalid_once) {
_pos_sp_triplet_published_invalid_once = true;
_pos_sp_triplet.previous.valid = false;
_pos_sp_triplet.current.valid = false;
_pos_sp_triplet.next.valid = false;
_pos_sp_triplet_updated = true;
}
if (_pos_sp_triplet_updated) {
_pos_sp_triplet.timestamp = hrt_absolute_time();
publish_position_setpoint_triplet();
_pos_sp_triplet_updated = false;
}
if (_mission_result_updated) {
publish_mission_result();
_mission_result_updated = false;
}
perf_end(_loop_perf);
}
PX4_INFO("exiting");
_navigator_task = -1;
}
PX4Magnetometer::~PX4Magnetometer()
{
if (_topic != nullptr) {
orb_unadvertise(_topic);
}
}
void *multirotor_position_control_thread_main()
{
/* welcome user */
fprintf (stdout, "Multirotor position controller started\n");
fflush(stdout);
int i;
bool_t updated;
bool_t reset_mission_sp = 0 /* false */;
bool_t global_pos_sp_valid = 0 /* false */;
bool_t reset_man_sp_z = 1 /* true */;
bool_t reset_man_sp_xy = 1 /* true */;
bool_t reset_int_z = 1 /* true */;
bool_t reset_int_z_manual = 0 /* false */;
bool_t reset_int_xy = 1 /* true */;
bool_t was_armed = 0 /* false */;
bool_t reset_auto_sp_xy = 1 /* true */;
bool_t reset_auto_sp_z = 1 /* true */;
bool_t reset_takeoff_sp = 1 /* true */;
absolute_time t_prev = 0;
const float alt_ctl_dz = 0.2f;
const float pos_ctl_dz = 0.05f;
float i_limit; /* use integral_limit_out = tilt_max / 2 */
float ref_alt = 0.0f;
absolute_time ref_alt_t = 0;
absolute_time local_ref_timestamp = 0;
PID_t xy_pos_pids[2];
PID_t xy_vel_pids[2];
PID_t z_pos_pid;
thrust_pid_t z_vel_pid;
float thrust_sp[3] = { 0.0f, 0.0f, 0.0f };
/* structures */
struct parameter_update_s ps;
struct vehicle_control_flags_s control_flags;
memset(&control_flags, 0, sizeof(control_flags));
struct vehicle_attitude_s att;
memset(&att, 0, sizeof(att));
struct vehicle_attitude_setpoint_s att_sp;
memset(&att_sp, 0, sizeof(att_sp));
struct manual_control_setpoint_s manual;
memset(&manual, 0, sizeof(manual));
struct vehicle_local_position_s local_pos;
memset(&local_pos, 0, sizeof(local_pos));
struct vehicle_local_position_setpoint_s local_pos_sp;
memset(&local_pos_sp, 0, sizeof(local_pos_sp));
struct vehicle_global_position_setpoint_s global_pos_sp;
memset(&global_pos_sp, 0, sizeof(global_pos_sp));
struct vehicle_global_velocity_setpoint_s global_vel_sp;
memset(&global_vel_sp, 0, sizeof(global_vel_sp));
/* subscribe to attitude, motor setpoints and system state */
orb_subscr_t param_sub = orb_subscribe(ORB_ID(parameter_update));
if (param_sub < 0)
{
fprintf (stderr, "Position controller thread failed to subscribe to parameter_update topic\n");
exit(-1);
}
orb_subscr_t control_flags_sub = orb_subscribe(ORB_ID(vehicle_control_flags));
if (control_flags_sub < 0)
{
fprintf (stderr, "Position controller thread failed to subscribe to vehicle_control_flags topic\n");
exit(-1);
}
orb_subscr_t att_sub = orb_subscribe(ORB_ID(vehicle_attitude));
if (att_sub < 0)
{
fprintf (stderr, "Position controller thread failed to subscribe to vehicle_attitude topic\n");
exit(-1);
}
orb_subscr_t att_sp_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint));
if (att_sp_sub < 0)
{
fprintf (stderr, "Position controller thread failed to subscribe to vehicle_attitude_setpoint topic\n");
exit(-1);
}
orb_subscr_t manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint));
if (manual_sub < 0)
{
fprintf (stderr, "Position controller thread failed to subscribe to manual_control_setpoint topic\n");
exit(-1);
}
orb_subscr_t local_pos_sp_sub = orb_subscribe(ORB_ID(vehicle_local_position_setpoint));
if (local_pos_sp_sub < 0)
{
fprintf (stderr, "Position controller thread failed to subscribe to vehicle_local_position_setpoint topic\n");
exit(-1);
}
orb_subscr_t local_pos_sub = orb_subscribe(ORB_ID(vehicle_local_position));
if (local_pos_sub < 0)
{
fprintf (stderr, "Position controller thread failed to subscribe to vehicle_local_position topic\n");
exit(-1);
}
orb_subscr_t global_pos_sp_sub = orb_subscribe(ORB_ID(vehicle_global_position_setpoint));
if (global_pos_sp_sub < 0)
{
fprintf (stderr, "Position controller thread failed to subscribe to vehicle_global_position_setpoint topic\n");
exit(-1);
}
/* publish setpoint */
orb_advert_t local_pos_sp_pub = orb_advertise(ORB_ID(vehicle_local_position_setpoint));
if (local_pos_sp_pub == -1)
{
fprintf (stderr, "Comunicator thread failed to advertise the vehicle_local_position_setpoint topic\n");
exit (-1);
}
orb_publish(ORB_ID(vehicle_local_position_setpoint), local_pos_sp_pub, &local_pos_sp);
orb_advert_t global_vel_sp_pub = orb_advertise(ORB_ID(vehicle_global_velocity_setpoint));
if (global_vel_sp_pub == -1)
{
fprintf (stderr, "Comunicator thread failed to advertise the vehicle_global_velocity_setpoint topic\n");
exit (-1);
}
orb_publish(ORB_ID(vehicle_global_velocity_setpoint), global_vel_sp_pub, &global_vel_sp);
orb_advert_t att_sp_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint));
if (att_sp_pub == -1)
{
fprintf (stderr, "Comunicator thread failed to advertise the vehicle_attitude_setpoint topic\n");
exit (-1);
}
orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp);
/* abort on a nonzero return value from the parameter init */
if (multirotor_position_control_params_init() != 0) {
/* parameter setup went wrong, abort */
fprintf (stderr, "Multirotor position controller aborting on startup due to an error\n");
exit(-1);
}
for (i = 0; i < 2; i++) {
pid_init(&(xy_pos_pids[i]), multirotor_position_control_parameters.xy_p, 0.0f,
multirotor_position_control_parameters.xy_d, 1.0f, 0.0f, PID_MODE_DERIVATIV_SET, 0.02f);
pid_init(&(xy_vel_pids[i]), multirotor_position_control_parameters.xy_vel_p, multirotor_position_control_parameters.xy_vel_i,
multirotor_position_control_parameters.xy_vel_d, 1.0f, multirotor_position_control_parameters.tilt_max, PID_MODE_DERIVATIV_CALC_NO_SP, 0.02f);
}
pid_init(&z_pos_pid, multirotor_position_control_parameters.z_p, 0.0f,
multirotor_position_control_parameters.z_d, 1.0f, multirotor_position_control_parameters.z_vel_max, PID_MODE_DERIVATIV_SET, 0.02f);
thrust_pid_init(&z_vel_pid, multirotor_position_control_parameters.z_vel_p, multirotor_position_control_parameters.z_vel_i,
multirotor_position_control_parameters.z_vel_d, -multirotor_position_control_parameters.thr_max, -multirotor_position_control_parameters.thr_min, PID_MODE_DERIVATIV_CALC_NO_SP, 0.02f);
while (!_shutdown_all_systems) {
updated = orb_check (ORB_ID(parameter_update), param_sub);
if (updated) {
/* clear updated flag */
orb_copy(ORB_ID(parameter_update), param_sub, &ps);
/* update multirotor_position_control_parameters */
multirotor_position_control_params_update();
for (i = 0; i < 2; i++) {
pid_set_parameters(&(xy_pos_pids[i]), multirotor_position_control_parameters.xy_p,
0.0f, multirotor_position_control_parameters.xy_d, 1.0f, 0.0f);
if (multirotor_position_control_parameters.xy_vel_i > 0.0f) {
i_limit = multirotor_position_control_parameters.tilt_max / multirotor_position_control_parameters.xy_vel_i / 2.0f;
} else {
i_limit = 0.0f; // not used
}
pid_set_parameters(&(xy_vel_pids[i]), multirotor_position_control_parameters.xy_vel_p,
multirotor_position_control_parameters.xy_vel_i, multirotor_position_control_parameters.xy_vel_d, i_limit, multirotor_position_control_parameters.tilt_max);
}
pid_set_parameters(&z_pos_pid, multirotor_position_control_parameters.z_p, 0.0f,
multirotor_position_control_parameters.z_d, 1.0f, multirotor_position_control_parameters.z_vel_max);
thrust_pid_set_parameters(&z_vel_pid, multirotor_position_control_parameters.z_vel_p, multirotor_position_control_parameters.z_vel_i,
multirotor_position_control_parameters.z_vel_d, -multirotor_position_control_parameters.thr_max, -multirotor_position_control_parameters.thr_min);
}
updated = orb_check (ORB_ID(vehicle_control_flags), control_flags_sub);
if (updated) {
orb_copy(ORB_ID(vehicle_control_flags), control_flags_sub, &control_flags);
}
updated = orb_check (ORB_ID(vehicle_global_position_setpoint), global_pos_sp_sub);
if (updated) {
orb_copy(ORB_ID(vehicle_global_position_setpoint), global_pos_sp_sub, &global_pos_sp);
global_pos_sp_valid = 1 /* true */;
reset_mission_sp = 1 /* true */;
}
absolute_time t = get_absolute_time();
float dt;
if (t_prev != 0) {
dt = (t - t_prev) * 0.000001f;
} else {
dt = 0.0f;
}
if (control_flags.flag_armed && !was_armed) {
/* reset setpoints and integrals on arming */
reset_man_sp_z = 1 /* true */;
reset_man_sp_xy = 1 /* true */;
reset_auto_sp_z = 1 /* true */;
reset_auto_sp_xy = 1 /* true */;
reset_takeoff_sp = 1 /* true */;
reset_int_z = 1 /* true */;
reset_int_xy = 1 /* true */;
}
was_armed = control_flags.flag_armed;
t_prev = t;
if (control_flags.flag_control_altitude_enabled || control_flags.flag_control_velocity_enabled || control_flags.flag_control_position_enabled) {
orb_copy(ORB_ID(manual_control_setpoint), manual_sub, &manual);
orb_copy(ORB_ID(vehicle_attitude), att_sub, &att);
orb_copy(ORB_ID(vehicle_attitude_setpoint), att_sp_sub, &att_sp);
orb_copy(ORB_ID(vehicle_local_position), local_pos_sub, &local_pos);
float z_sp_offs_max = multirotor_position_control_parameters.z_vel_max / multirotor_position_control_parameters.z_p * 2.0f;
float xy_sp_offs_max = multirotor_position_control_parameters.xy_vel_max / multirotor_position_control_parameters.xy_p * 2.0f;
float sp_move_rate[3] = { 0.0f, 0.0f, 0.0f };
if (control_flags.flag_control_manual_enabled) {
/* manual control */
/* check for reference point updates and correct setpoint */
if (local_pos.ref_timestamp != ref_alt_t) {
if (ref_alt_t != 0) {
/* home alt changed, don't follow large ground level changes in manual flight */
local_pos_sp.z += local_pos.ref_alt - ref_alt;
}
ref_alt_t = local_pos.ref_timestamp;
ref_alt = local_pos.ref_alt;
// TODO also correct XY setpoint
}
/* reset setpoints to current position if needed */
if (control_flags.flag_control_altitude_enabled) {
if (reset_man_sp_z) {
reset_man_sp_z = 0 /* false */;
local_pos_sp.z = local_pos.z;
//mavlink_log_info(mavlink_fd, "[mpc] reset alt sp: %.2f", (double) - local_pos_sp.z);
}
/* move altitude setpoint with throttle stick */
float z_sp_ctl = scale_control(manual.thrust - 0.5f, 0.5f, alt_ctl_dz);
if (z_sp_ctl != 0.0f) {
sp_move_rate[2] = -z_sp_ctl * multirotor_position_control_parameters.z_vel_max;
local_pos_sp.z += sp_move_rate[2] * dt;
if (local_pos_sp.z > local_pos.z + z_sp_offs_max) {
local_pos_sp.z = local_pos.z + z_sp_offs_max;
} else if (local_pos_sp.z < local_pos.z - z_sp_offs_max) {
local_pos_sp.z = local_pos.z - z_sp_offs_max;
}
}
}
if (control_flags.flag_control_position_enabled) {
if (reset_man_sp_xy) {
reset_man_sp_xy = 0 /* false */;
local_pos_sp.x = local_pos.x;
local_pos_sp.y = local_pos.y;
pid_reset_integral(&xy_vel_pids[0]);
pid_reset_integral(&xy_vel_pids[1]);
//mavlink_log_info(mavlink_fd, "[mpc] reset pos sp: %.2f, %.2f", (double)local_pos_sp.x, (double)local_pos_sp.y);
}
/* move position setpoint with roll/pitch stick */
float pos_pitch_sp_ctl = scale_control(-manual.pitch / multirotor_position_control_parameters.rc_scale_pitch, 1.0f, pos_ctl_dz);
float pos_roll_sp_ctl = scale_control(manual.roll / multirotor_position_control_parameters.rc_scale_roll, 1.0f, pos_ctl_dz);
if (pos_pitch_sp_ctl != 0.0f || pos_roll_sp_ctl != 0.0f) {
/* calculate direction and increment of control in NED frame */
float xy_sp_ctl_dir = att.yaw + atan2f(pos_roll_sp_ctl, pos_pitch_sp_ctl);
float xy_sp_ctl_speed = norm(pos_pitch_sp_ctl, pos_roll_sp_ctl) * multirotor_position_control_parameters.xy_vel_max;
sp_move_rate[0] = cosf(xy_sp_ctl_dir) * xy_sp_ctl_speed;
sp_move_rate[1] = sinf(xy_sp_ctl_dir) * xy_sp_ctl_speed;
local_pos_sp.x += sp_move_rate[0] * dt;
local_pos_sp.y += sp_move_rate[1] * dt;
/* limit maximum setpoint from position offset and preserve direction
* fail safe, should not happen in normal operation */
float pos_vec_x = local_pos_sp.x - local_pos.x;
float pos_vec_y = local_pos_sp.y - local_pos.y;
float pos_vec_norm = norm(pos_vec_x, pos_vec_y) / xy_sp_offs_max;
if (pos_vec_norm > 1.0f) {
local_pos_sp.x = local_pos.x + pos_vec_x / pos_vec_norm;
local_pos_sp.y = local_pos.y + pos_vec_y / pos_vec_norm;
}
}
}
/* copy yaw setpoint to vehicle_local_position_setpoint topic */
local_pos_sp.yaw = att_sp.yaw_body;
/* local position setpoint is valid and can be used for auto loiter after position controlled mode */
reset_auto_sp_xy = !control_flags.flag_control_position_enabled;
reset_auto_sp_z = !control_flags.flag_control_altitude_enabled;
reset_takeoff_sp = 1 /* true */;
/* force reprojection of global setpoint after manual mode */
reset_mission_sp = 1 /* true */;
} else if (control_flags.flag_control_auto_enabled) {
/* AUTO mode, use global setpoint */
if (control_flags.auto_state == navigation_state_auto_ready) {
reset_auto_sp_xy = 1 /* true */;
reset_auto_sp_z = 1 /* true */;
} else if (control_flags.auto_state == navigation_state_auto_takeoff) {
if (reset_takeoff_sp) {
reset_takeoff_sp = 0 /* false */;
local_pos_sp.x = local_pos.x;
local_pos_sp.y = local_pos.y;
local_pos_sp.z = - multirotor_position_control_parameters.takeoff_alt - multirotor_position_control_parameters.takeoff_gap;
att_sp.yaw_body = att.yaw;
//mavlink_log_info(mavlink_fd, "[mpc] takeoff sp: %.2f %.2f %.2f", (double)local_pos_sp.x, (double)local_pos_sp.y, (double) - local_pos_sp.z);
}
reset_auto_sp_xy = 0 /* false */;
reset_auto_sp_z = 1 /* true */;
} else if (control_flags.auto_state == navigation_state_auto_rtl) {
// TODO
reset_auto_sp_xy = 1 /* true */;
reset_auto_sp_z = 1 /* true */;
} else if (control_flags.auto_state == navigation_state_auto_mission) {
/* init local projection using local position ref */
if (local_pos.ref_timestamp != local_ref_timestamp) {
reset_mission_sp = 1 /* true */;
local_ref_timestamp = local_pos.ref_timestamp;
double lat_home = local_pos.ref_lat * 1e-7;
double lon_home = local_pos.ref_lon * 1e-7;
map_projection_init(lat_home, lon_home);
//mavlink_log_info(mavlink_fd, "[mpc] local pos ref: %.7f, %.7f", (double)lat_home, (double)lon_home);
}
if (reset_mission_sp) {
reset_mission_sp = 0 /* false */;
/* update global setpoint projection */
if (global_pos_sp_valid) {
/* global position setpoint valid, use it */
double sp_lat = global_pos_sp.latitude * 1e-7;
double sp_lon = global_pos_sp.longitude * 1e-7;
/* project global setpoint to local setpoint */
map_projection_project(sp_lat, sp_lon, &(local_pos_sp.x), &(local_pos_sp.y));
if (global_pos_sp.altitude_is_relative) {
local_pos_sp.z = -global_pos_sp.altitude;
} else {
local_pos_sp.z = local_pos.ref_alt - global_pos_sp.altitude;
}
att_sp.yaw_body = global_pos_sp.yaw;
//mavlink_log_info(mavlink_fd, "[mpc] new sp: %.7f, %.7f (%.2f, %.2f)", (double)sp_lat, sp_lon, (double)local_pos_sp.x, (double)local_pos_sp.y);
} else {
if (reset_auto_sp_xy) {
reset_auto_sp_xy = 0 /* false */;
/* local position setpoint is invalid,
* use current position as setpoint for loiter */
local_pos_sp.x = local_pos.x;
local_pos_sp.y = local_pos.y;
local_pos_sp.yaw = att.yaw;
}
if (reset_auto_sp_z) {
reset_auto_sp_z = 0 /* false */;
local_pos_sp.z = local_pos.z;
}
//mavlink_log_info(mavlink_fd, "[mpc] no global pos sp, loiter: %.2f, %.2f", (double)local_pos_sp.x, (double)local_pos_sp.y);
}
}
reset_auto_sp_xy = 1 /* true */;
reset_auto_sp_z = 1 /* true */;
}
if (control_flags.auto_state != navigation_state_auto_takeoff) {
reset_takeoff_sp = 1 /* true */;
}
if (control_flags.auto_state != navigation_state_auto_mission) {
reset_mission_sp = 1 /* true */;
}
/* copy yaw setpoint to vehicle_local_position_setpoint topic */
local_pos_sp.yaw = att_sp.yaw_body;
/* reset setpoints after AUTO mode */
reset_man_sp_xy = 1 /* true */;
reset_man_sp_z = 1 /* true */;
} else {
/* no control (failsafe), loiter or stay on ground */
if (local_pos.landed) {
/* landed: move setpoint down */
/* in air: hold altitude */
if (local_pos_sp.z < 5.0f) {
/* set altitude setpoint to 5m under ground,
* don't set it too deep to avoid unexpected landing in case of false "landed" signal */
local_pos_sp.z = 5.0f;
//mavlink_log_info(mavlink_fd, "[mpc] landed, set alt: %.2f", (double) - local_pos_sp.z);
}
reset_man_sp_z = 1 /* true */;
} else {
/* in air: hold altitude */
if (reset_man_sp_z) {
reset_man_sp_z = 0 /* false */;
local_pos_sp.z = local_pos.z;
//mavlink_log_info(mavlink_fd, "[mpc] set loiter alt: %.2f", (double) - local_pos_sp.z);
}
reset_auto_sp_z = 0 /* false */;
}
if (control_flags.flag_control_position_enabled) {
if (reset_man_sp_xy) {
reset_man_sp_xy = 0 /* false */;
local_pos_sp.x = local_pos.x;
local_pos_sp.y = local_pos.y;
local_pos_sp.yaw = att.yaw;
att_sp.yaw_body = att.yaw;
//mavlink_log_info(mavlink_fd, "[mpc] set loiter pos: %.2f %.2f", (double)local_pos_sp.x, (double)local_pos_sp.y);
}
reset_auto_sp_xy = 0 /* false */;
}
}
/* publish local position setpoint */
orb_publish(ORB_ID(vehicle_local_position_setpoint), local_pos_sp_pub, &local_pos_sp);
/* run position & altitude controllers, calculate velocity setpoint */
if (control_flags.flag_control_altitude_enabled) {
global_vel_sp.vz = pid_calculate(&z_pos_pid, local_pos_sp.z, local_pos.z, local_pos.vz - sp_move_rate[2], dt) + sp_move_rate[2];
} else {
reset_man_sp_z = 1 /* true */;
global_vel_sp.vz = 0.0f;
}
if (control_flags.flag_control_position_enabled) {
/* calculate velocity set point in NED frame */
global_vel_sp.vx = pid_calculate(&xy_pos_pids[0], local_pos_sp.x, local_pos.x, local_pos.vx - sp_move_rate[0], dt) + sp_move_rate[0];
global_vel_sp.vy = pid_calculate(&xy_pos_pids[1], local_pos_sp.y, local_pos.y, local_pos.vy - sp_move_rate[1], dt) + sp_move_rate[1];
/* limit horizontal speed */
float xy_vel_sp_norm = norm(global_vel_sp.vx, global_vel_sp.vy) / multirotor_position_control_parameters.xy_vel_max;
if (xy_vel_sp_norm > 1.0f) {
global_vel_sp.vx /= xy_vel_sp_norm;
global_vel_sp.vy /= xy_vel_sp_norm;
}
} else {
reset_man_sp_xy = 1 /* true */;
global_vel_sp.vx = 0.0f;
global_vel_sp.vy = 0.0f;
}
//fprintf (stderr, "global_vel_sp.vx:%.3f\tglobal_vel_sp.vy:%.3f\tglobal_vel_sp.vz:%.3f\n", global_vel_sp.vx, global_vel_sp.vy, global_vel_sp.vz);
/* publish new velocity setpoint */
orb_publish(ORB_ID(vehicle_global_velocity_setpoint), global_vel_sp_pub, &global_vel_sp);
// TODO subscribe to velocity setpoint if altitude/position control disabled
if (control_flags.flag_control_climb_rate_enabled || control_flags.flag_control_velocity_enabled) {
/* run velocity controllers, calculate thrust vector with attitude-thrust compensation */
if (control_flags.flag_control_climb_rate_enabled) {
if (reset_int_z) {
reset_int_z = 0 /* false */;
float i = multirotor_position_control_parameters.thr_min;
if (reset_int_z_manual) {
i = manual.thrust;
if (i < multirotor_position_control_parameters.thr_min) {
i = multirotor_position_control_parameters.thr_min;
} else if (i > multirotor_position_control_parameters.thr_max) {
i = multirotor_position_control_parameters.thr_max;
}
}
thrust_pid_set_integral(&z_vel_pid, -i);
//mavlink_log_info(mavlink_fd, "[mpc] reset hovering thrust: %.2f", (double)i);
}
thrust_sp[2] = thrust_pid_calculate(&z_vel_pid, global_vel_sp.vz, local_pos.vz, dt, att.R[2][2]);
att_sp.thrust = -thrust_sp[2];
} else {
/* reset thrust integral when altitude control enabled */
reset_int_z = 1 /* true */;
}
if (control_flags.flag_control_velocity_enabled) {
/* calculate thrust set point in NED frame */
if (reset_int_xy) {
reset_int_xy = 0 /* false */;
pid_reset_integral(&xy_vel_pids[0]);
pid_reset_integral(&xy_vel_pids[1]);
//mavlink_log_info(mavlink_fd, "[mpc] reset pos integral");
}
thrust_sp[0] = pid_calculate(&xy_vel_pids[0], global_vel_sp.vx, local_pos.vx, 0.0f, dt);
thrust_sp[1] = pid_calculate(&xy_vel_pids[1], global_vel_sp.vy, local_pos.vy, 0.0f, dt);
/* thrust_vector now contains desired acceleration (but not in m/s^2) in NED frame */
/* limit horizontal part of thrust */
float thrust_xy_dir = atan2f(thrust_sp[1], thrust_sp[0]);
/* assuming that vertical component of thrust is g,
* horizontal component = g * tan(alpha) */
float tilt = atanf(norm(thrust_sp[0], thrust_sp[1]));
if (tilt > multirotor_position_control_parameters.tilt_max) {
tilt = multirotor_position_control_parameters.tilt_max;
}
/* convert direction to body frame */
thrust_xy_dir -= att.yaw;
/* calculate roll and pitch */
att_sp.roll_body = sinf(thrust_xy_dir) * tilt;
att_sp.pitch_body = -cosf(thrust_xy_dir) * tilt / cosf(att_sp.roll_body);
} else {
reset_int_xy = 1 /* true */;
}
att_sp.timestamp = get_absolute_time();
//fprintf (stderr, "att_sp.roll:%.3f\tatt_sp.pitch:%.3f\tatt_sp.yaw:%.3f\tatt_sp.thrust:%.3f\n", att_sp.roll_body, att_sp.pitch_body, att_sp.yaw_body, att_sp.thrust);
/* publish new attitude setpoint */
orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp);
}
} else {
/* position controller disabled, reset setpoints */
reset_man_sp_z = 1 /* true */;
reset_man_sp_xy = 1 /* true */;
reset_int_z = 1 /* true */;
reset_int_xy = 1 /* true */;
reset_mission_sp = 1 /* true */;
reset_auto_sp_xy = 1 /* true */;
reset_auto_sp_z = 1 /* true */;
}
/* reset altitude controller integral (hovering throttle) to manual throttle after manual throttle control */
reset_int_z_manual = control_flags.flag_armed && control_flags.flag_control_manual_enabled && !control_flags.flag_control_climb_rate_enabled;
/* run at approximately 50 Hz */
usleep(20000);
}
/*
* do unsubscriptions
*/
orb_unsubscribe(ORB_ID(parameter_update), param_sub, pthread_self());
orb_unsubscribe(ORB_ID(vehicle_control_flags), control_flags_sub, pthread_self());
orb_unsubscribe(ORB_ID(vehicle_attitude), att_sub, pthread_self());
orb_unsubscribe(ORB_ID(vehicle_attitude_setpoint), att_sp_sub, pthread_self());
orb_unsubscribe(ORB_ID(manual_control_setpoint), manual_sub, pthread_self());
orb_unsubscribe(ORB_ID(vehicle_local_position_setpoint), local_pos_sp_sub, pthread_self());
orb_unsubscribe(ORB_ID(vehicle_local_position), local_pos_sub, pthread_self());
orb_unsubscribe(ORB_ID(vehicle_global_position_setpoint), global_pos_sp_sub, pthread_self());
/*
* do unadvertises
*/
orb_unadvertise(ORB_ID(vehicle_local_position_setpoint), local_pos_sp_pub, pthread_self());
orb_unadvertise(ORB_ID(vehicle_global_velocity_setpoint), global_vel_sp_pub, pthread_self());
orb_unadvertise(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, pthread_self());
return 0;
}
