mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-19 13:13:34 +08:00
Massive improvements in state machine, still tracing wrong throttle scaling in manual input path
This commit is contained in:
+47
-47
@@ -230,11 +230,11 @@ void cal_bsort(int16_t a[], int n)
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}
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}
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void do_mag_calibration(int status_pub, struct vehicle_status_s *current_status)
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void do_mag_calibration(int status_pub, struct vehicle_status_s *status)
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{
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/* set to mag calibration mode */
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current_status->preflight_mag_calibration = true;
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state_machine_publish(status_pub, current_status);
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status->preflight_mag_calibration = true;
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state_machine_publish(status_pub, status, mavlink_fd);
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int sub_sensor_combined = orb_subscribe(ORB_ID(sensor_combined));
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struct sensor_combined_s raw;
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@@ -312,8 +312,8 @@ void do_mag_calibration(int status_pub, struct vehicle_status_s *current_status)
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}
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/* disable calibration mode */
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current_status->preflight_mag_calibration = false;
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state_machine_publish(status_pub, current_status);
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status->preflight_mag_calibration = false;
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state_machine_publish(status_pub, status, mavlink_fd);
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/* sort values */
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cal_bsort(mag_minima[0], peak_samples);
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@@ -393,7 +393,7 @@ void do_mag_calibration(int status_pub, struct vehicle_status_s *current_status)
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free(mag_minima[2]);
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char offset_output[50];
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sprintf(offset_output, "[commander] mag calibration finished, offsets: x:%d, y:%d, z:%d", mag_offset[0], mag_offset[1], mag_offset[2]);
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sprintf(offset_output, "[commander] mag cal: x:%8.4f y:%8.4f z:%8.4f", (double)mag_offset[0], (double)mag_offset[1], (double)mag_offset[2]);
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mavlink_log_info(mavlink_fd, offset_output);
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close(sub_sensor_combined);
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@@ -436,7 +436,7 @@ void do_gyro_calibration(int status_pub, struct vehicle_status_s *current_status
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global_data_parameter_storage->pm.param_values[PARAM_SENSOR_GYRO_ZOFFSET] = gyro_offset[2];
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char offset_output[50];
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sprintf(offset_output, "[commander] gyro calibration finished, offsets: x:%d, y:%d, z:%d", (int)gyro_offset[0], (int)gyro_offset[1], (int)gyro_offset[2]);
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sprintf(offset_output, "[commander] gyro cal: x:%8.4f y:%8.4f z:%8.4f", (double)gyro_offset[0], (double)gyro_offset[1], (double)gyro_offset[2]);
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mavlink_log_info(mavlink_fd, offset_output);
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close(sub_sensor_combined);
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@@ -458,7 +458,7 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
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switch (cmd->command) {
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case MAV_CMD_DO_SET_MODE:
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{
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if (OK == update_state_machine_mode_request(status_pub, current_vehicle_status, (uint8_t)cmd->param1)) {
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if (OK == update_state_machine_mode_request(status_pub, current_vehicle_status, mavlink_fd, (uint8_t)cmd->param1)) {
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result = MAV_RESULT_ACCEPTED;
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} else {
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result = MAV_RESULT_DENIED;
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@@ -466,18 +466,17 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
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}
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break;
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case MAV_CMD_COMPONENT_ARM_DISARM:
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{
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case MAV_CMD_COMPONENT_ARM_DISARM: {
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/* request to arm */
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if ((int)cmd->param1 == 1) {
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if (OK == update_state_machine_mode_request(status_pub, current_vehicle_status, VEHICLE_MODE_FLAG_SAFETY_ARMED)) {
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if (OK == update_state_machine_mode_request(status_pub, current_vehicle_status, mavlink_fd, VEHICLE_MODE_FLAG_SAFETY_ARMED)) {
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result = MAV_RESULT_ACCEPTED;
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} else {
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result = MAV_RESULT_DENIED;
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}
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/* request to disarm */
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} else if ((int)cmd->param1 == 0) {
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if (OK == update_state_machine_mode_request(status_pub, current_vehicle_status, VEHICLE_MODE_FLAG_SAFETY_ARMED)) {
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if (OK == update_state_machine_mode_request(status_pub, current_vehicle_status, mavlink_fd, VEHICLE_MODE_FLAG_SAFETY_ARMED)) {
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result = MAV_RESULT_ACCEPTED;
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} else {
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result = MAV_RESULT_DENIED;
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@@ -487,19 +486,19 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
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break;
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/* request for an autopilot reboot */
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case MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN:
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{
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// if ((int)cmd->param1 == 1) {
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// if (OK == update_state_machine_custom_mode_request(status_pub, current_vehicle_status, SYSTEM_STATE_HALT)) {
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// result = MAV_RESULT_ACCEPTED;//TODO: this has no effect
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// } else {
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// result = MAV_RESULT_DENIED;
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// }
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// }
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case MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN: {
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if ((int)cmd->param1 == 1) {
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if (OK == do_state_update(status_pub, current_vehicle_status, mavlink_fd, SYSTEM_STATE_REBOOT)) {
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/* SPECIAL CASE: SYSTEM WILL NEVER RETURN HERE */
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result = MAV_RESULT_ACCEPTED;
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} else {
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/* system may return here */
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result = MAV_RESULT_DENIED;
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}
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}
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}
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break;
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//
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// /* request to land */
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// case MAV_CMD_NAV_LAND:
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// {
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@@ -524,18 +523,18 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
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// break;
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//
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/* preflight calibration */
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case MAV_CMD_PREFLIGHT_CALIBRATION: {
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case MAV_CMD_PREFLIGHT_CALIBRATION: {
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bool handled = false;
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/* gyro calibration */
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if ((int)(cmd->param1) == 1) {
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/* transition to calibration state */
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do_state_update(status_pub, ¤t_status, SYSTEM_STATE_PREFLIGHT);
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do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_PREFLIGHT);
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if (current_status.state_machine == SYSTEM_STATE_PREFLIGHT) {
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mavlink_log_info(mavlink_fd, "[commander] starting gyro calibration");
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do_gyro_calibration(status_pub, ¤t_status);
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do_state_update(status_pub, ¤t_status, SYSTEM_STATE_STANDBY);
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do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_STANDBY);
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result = MAV_RESULT_ACCEPTED;
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} else {
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mavlink_log_critical(mavlink_fd, "[commander] REJECTING gyro calibration");
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@@ -547,12 +546,12 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
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/* magnetometer calibration */
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if ((int)(cmd->param2) == 1) {
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/* transition to calibration state */
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do_state_update(status_pub, ¤t_status, SYSTEM_STATE_PREFLIGHT);
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do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_PREFLIGHT);
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if (current_status.state_machine == SYSTEM_STATE_PREFLIGHT) {
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mavlink_log_info(mavlink_fd, "[commander] starting mag calibration");
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do_mag_calibration(status_pub, ¤t_status);
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do_state_update(status_pub, ¤t_status, SYSTEM_STATE_STANDBY);
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do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_STANDBY);
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result = MAV_RESULT_ACCEPTED;
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} else {
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mavlink_log_critical(mavlink_fd, "[commander] REJECTING mag calibration");
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@@ -571,7 +570,7 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
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break;
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/* preflight parameter load / store */
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case MAV_CMD_PREFLIGHT_STORAGE: {
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case MAV_CMD_PREFLIGHT_STORAGE: {
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/* Read all parameters from EEPROM to RAM */
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if (((int)cmd->param1) == 0) {
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@@ -610,7 +609,7 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
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}
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break;
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default: {
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default: {
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mavlink_log_critical(mavlink_fd, "[commander] refusing unsupported command");
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result = MAV_RESULT_UNSUPPORTED;
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}
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@@ -625,8 +624,6 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
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/* send acknowledge command */
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mavlink_message_t msg;
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mavlink_msg_command_ack_pack(0, 0, &msg, cmd->command, result);
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//global_data_send_mavlink_message_out(&msg);
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}
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}
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@@ -736,6 +733,8 @@ enum BAT_CHEM {
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*
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* @return the estimated remaining capacity in 0..1
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*/
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float battery_remaining_estimate_voltage(int cells, int chemistry, float voltage);
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float battery_remaining_estimate_voltage(int cells, int chemistry, float voltage)
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{
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float ret = 0;
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@@ -783,17 +782,19 @@ int commander_main(int argc, char *argv[])
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fprintf(stderr, "[commander] ERROR: Failed to open MAVLink log stream, start mavlink app first.\n");
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}
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/* make sure we are in preflight state */
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memset(¤t_status, 0, sizeof(current_status));
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current_status.state_machine = SYSTEM_STATE_PREFLIGHT;
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/* advertise to ORB */
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stat_pub = orb_advertise(ORB_ID(vehicle_status), ¤t_status);
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state_machine_publish(stat_pub, ¤t_status, mavlink_fd);
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if (stat_pub < 0) {
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printf("[commander] ERROR: orb_advertise for topic vehicle_status failed.\n");
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exit(ERROR);
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}
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/* make sure we are in preflight state */
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//do_state_update(stat_pub, ¤t_status, (commander_state_machine_t)SYSTEM_STATE_PREFLIGHT);
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mavlink_log_info(mavlink_fd, "[commander] system is running");
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/* load EEPROM parameters */
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@@ -854,11 +855,10 @@ int commander_main(int argc, char *argv[])
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struct sensor_combined_s sensors;
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memset(&sensors, 0, sizeof(sensors));
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uint8_t vehicle_state_previous = current_status.state_machine;
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// uint8_t vehicle_state_previous = current_status.state_machine;
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float voltage_previous = 0.0f;
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uint64_t last_idle_time = 0;
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unsigned int signal_loss_counter = 0;
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/* now initialized */
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commander_initialized = true;
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@@ -891,7 +891,7 @@ int commander_main(int argc, char *argv[])
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}
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/* toggle error led at 5 Hz in HIL mode */
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if ((current_status.mode & MAV_MODE_FLAG_HIL_ENABLED)) {
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if ((current_status.mode & VEHICLE_MODE_FLAG_HIL_ENABLED)) {
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/* armed */
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led_toggle(LED_AMBER);
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@@ -994,7 +994,7 @@ int commander_main(int argc, char *argv[])
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//
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//
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// if (flight_env == PX4_FLIGHT_ENVIRONMENT_TESTING) //simulate position fix for quick indoor tests
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update_state_machine_got_position_fix(stat_pub, ¤t_status);
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update_state_machine_got_position_fix(stat_pub, ¤t_status, mavlink_fd);
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/* end: check gps */
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/* Check battery voltage */
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@@ -1017,7 +1017,7 @@ int commander_main(int argc, char *argv[])
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if (critical_voltage_counter > CRITICAL_VOLTAGE_BATTERY_COUNTER_LIMIT) {
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critical_battery_voltage_actions_done = true;
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mavlink_log_critical(mavlink_fd, "[commander] EMERGENCY! CIRITICAL BATTERY!");
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state_machine_emergency(stat_pub, ¤t_status);
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state_machine_emergency(stat_pub, ¤t_status, mavlink_fd);
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}
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critical_voltage_counter++;
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@@ -1044,7 +1044,7 @@ int commander_main(int argc, char *argv[])
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/* check if left stick is in lower left position --> switch to standby state */
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if (rc_yaw_scale < -STICK_ON_OFF_LIMIT && rc_throttle_scale < STICK_THRUST_RANGE*0.2f) { //TODO: remove hardcoded values
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if (stick_off_counter > STICK_ON_OFF_COUNTER_LIMIT) {
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update_state_machine_disarm(stat_pub, ¤t_status);
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update_state_machine_disarm(stat_pub, ¤t_status, mavlink_fd);
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stick_on_counter = 0;
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} else {
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@@ -1056,7 +1056,7 @@ int commander_main(int argc, char *argv[])
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/* check if left stick is in lower right position --> arm */
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if (rc_yaw_scale > STICK_ON_OFF_LIMIT && rc_throttle_scale < STICK_THRUST_RANGE*0.2f) { //TODO: remove hardcoded values
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if (stick_on_counter > STICK_ON_OFF_COUNTER_LIMIT) {
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update_state_machine_arm(stat_pub, ¤t_status);
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update_state_machine_arm(stat_pub, ¤t_status, mavlink_fd);
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stick_on_counter = 0;
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} else {
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@@ -1067,13 +1067,13 @@ int commander_main(int argc, char *argv[])
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//printf("RC: y:%i/t:%i s:%i chans: %i\n", rc_yaw_scale, rc_throttle_scale, mode_switch_rc_value, rc.chan_count);
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if (mode_switch_rc_value > STICK_ON_OFF_LIMIT) {
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update_state_machine_mode_manual(stat_pub, ¤t_status);
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update_state_machine_mode_manual(stat_pub, ¤t_status, mavlink_fd);
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} else if (mode_switch_rc_value < -STICK_ON_OFF_LIMIT) {
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update_state_machine_mode_auto(stat_pub, ¤t_status);
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update_state_machine_mode_auto(stat_pub, ¤t_status, mavlink_fd);
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} else {
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update_state_machine_mode_stabilized(stat_pub, ¤t_status);
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update_state_machine_mode_stabilized(stat_pub, ¤t_status, mavlink_fd);
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}
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/* Publish RC signal */
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@@ -1112,11 +1112,11 @@ int commander_main(int argc, char *argv[])
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current_status.preflight_gyro_calibration == false &&
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current_status.preflight_mag_calibration == false) {
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/* All ok, no calibration going on, go to standby */
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do_state_update(stat_pub, ¤t_status, SYSTEM_STATE_STANDBY);
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do_state_update(stat_pub, ¤t_status, SYSTEM_STATE_STANDBY, mavlink_fd);
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}
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/* Store old modes to detect and act on state transitions */
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vehicle_state_previous = current_status.state_machine;
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// vehicle_state_previous = current_status.state_machine;
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voltage_previous = current_status.voltage_battery;
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fflush(stdout);
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@@ -45,6 +45,7 @@
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#include <uORB/topics/vehicle_status.h>
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#include <systemlib/systemlib.h>
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#include <arch/board/up_hrt.h>
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#include <mavlink/mavlink_log.h>
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static const char* system_state_txt[] = {
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"SYSTEM_STATE_PREFLIGHT",
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@@ -61,10 +62,13 @@ static const char* system_state_txt[] = {
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};
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void do_state_update(int status_pub, struct vehicle_status_s *current_status, commander_state_machine_t new_state)
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/**
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* Transition from one state to another
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*/
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int do_state_update(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, commander_state_machine_t new_state)
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{
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int invalid_state = false;
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int ret = ERROR;
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commander_state_machine_t old_state = current_status->state_machine;
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@@ -74,10 +78,10 @@ void do_state_update(int status_pub, struct vehicle_status_s *current_status, co
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uint8_t flight_environment_parameter = (uint8_t)(global_data_parameter_storage->pm.param_values[PARAM_FLIGHT_ENV]);
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if (flight_environment_parameter == PX4_FLIGHT_ENVIRONMENT_OUTDOOR) {
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do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_EMCY_LANDING);
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ret = do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_EMCY_LANDING);
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} else {
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do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_EMCY_CUTOFF);
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ret = do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_EMCY_CUTOFF);
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}
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return;
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@@ -89,63 +93,63 @@ void do_state_update(int status_pub, struct vehicle_status_s *current_status, co
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//TODO: add emcy landing code here
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fprintf(stderr, "[commander] EMERGENCY LANDING!\n");
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//global_data_send_mavlink_statustext_message_out("Commander: state: emergency landing", MAV_SEVERITY_INFO);
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mavlink_log_critical(mavlink_fd, "[commander] EMERGENCY LANDING!");
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break;
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case SYSTEM_STATE_EMCY_CUTOFF:
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/* Tell the controller to cutoff the motors (thrust = 0), make sure that this is not overwritten by another app and stays at 0 */
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//TODO: add emcy cutoff code here
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/* Tell the controller to cutoff the motors (thrust = 0) */
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fprintf(stderr, "[commander] EMERGENCY MOTOR CUTOFF!\n");
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//global_data_send_mavlink_statustext_message_out("Commander: state: emergency cutoff", MAV_SEVERITY_INFO);
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mavlink_log_critical(mavlink_fd, "[commander] EMERGENCY MOTOR CUTOFF!");
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break;
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case SYSTEM_STATE_GROUND_ERROR:
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fprintf(stderr, "[commander] GROUND ERROR, locking down propulsion system\n");
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//global_data_send_mavlink_statustext_message_out("Commander: state: ground error", MAV_SEVERITY_INFO);
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mavlink_log_critical(mavlink_fd, "[commander] GROUND ERROR, locking down propulsion system");
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break;
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case SYSTEM_STATE_PREFLIGHT:
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//global_data_send_mavlink_statustext_message_out("Commander: state: preflight", MAV_SEVERITY_INFO);
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if (current_status->state_machine == SYSTEM_STATE_STANDBY
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|| current_status->state_machine == SYSTEM_STATE_PREFLIGHT) {
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invalid_state = false;
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mavlink_log_info(mavlink_fd, "[commander] Switched to PREFLIGHT state");
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} else {
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invalid_state = true;
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mavlink_log_critical(mavlink_fd, "[commander] REFUSED to switch to PREFLIGHT state");
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}
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break;
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case SYSTEM_STATE_REBOOT:
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usleep(500000);
|
||||
reboot();
|
||||
if (current_status->state_machine == SYSTEM_STATE_STANDBY
|
||||
|| current_status->state_machine == SYSTEM_STATE_PREFLIGHT) {
|
||||
invalid_state = false;
|
||||
mavlink_log_critical(mavlink_fd, "[commander] REBOOTING SYSTEM");
|
||||
usleep(500000);
|
||||
reboot();
|
||||
/* SPECIAL CASE: NEVER RETURNS FROM THIS FUNCTION CALL */
|
||||
} else {
|
||||
invalid_state = true;
|
||||
mavlink_log_critical(mavlink_fd, "[commander] REFUSED to REBOOT");
|
||||
}
|
||||
break;
|
||||
|
||||
case SYSTEM_STATE_STANDBY:
|
||||
//global_data_send_mavlink_statustext_message_out("Commander: state: standby", MAV_SEVERITY_INFO);
|
||||
mavlink_log_critical(mavlink_fd, "[commander] Switched to STANDBY state");
|
||||
break;
|
||||
|
||||
case SYSTEM_STATE_GROUND_READY:
|
||||
//global_data_send_mavlink_statustext_message_out("Commander: state: armed", MAV_SEVERITY_INFO);
|
||||
|
||||
//if in manual mode switch to manual state
|
||||
// if (current_status->remote_manual) {
|
||||
// printf("[commander] manual mode\n");
|
||||
// do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_MANUAL);
|
||||
// return;
|
||||
// }
|
||||
|
||||
mavlink_log_critical(mavlink_fd, "[commander] Switched to GROUND READY state");
|
||||
break;
|
||||
|
||||
case SYSTEM_STATE_AUTO:
|
||||
//global_data_send_mavlink_statustext_message_out("Commander: state: auto", MAV_SEVERITY_INFO);
|
||||
mavlink_log_critical(mavlink_fd, "[commander] Switched to FLYING / AUTO mode");
|
||||
break;
|
||||
|
||||
case SYSTEM_STATE_STABILIZED:
|
||||
//global_data_send_mavlink_statustext_message_out("Commander: state: stabilized", MAV_SEVERITY_INFO);
|
||||
mavlink_log_critical(mavlink_fd, "[commander] Switched to FLYING / STABILIZED mode");
|
||||
break;
|
||||
|
||||
case SYSTEM_STATE_MANUAL:
|
||||
//global_data_send_mavlink_statustext_message_out("Commander: state: manual", MAV_SEVERITY_INFO);
|
||||
mavlink_log_critical(mavlink_fd, "[commander] Switched to FLYING / MANUAL mode");
|
||||
break;
|
||||
|
||||
default:
|
||||
@@ -155,11 +159,11 @@ void do_state_update(int status_pub, struct vehicle_status_s *current_status, co
|
||||
|
||||
if (invalid_state == false || old_state != new_state) {
|
||||
current_status->state_machine = new_state;
|
||||
state_machine_publish(status_pub, current_status);
|
||||
state_machine_publish(status_pub, current_status, mavlink_fd);
|
||||
}
|
||||
}
|
||||
|
||||
void state_machine_publish(int status_pub, struct vehicle_status_s *current_status) {
|
||||
void state_machine_publish(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) {
|
||||
/* publish the new state */
|
||||
current_status->counter++;
|
||||
current_status->timestamp = hrt_absolute_time();
|
||||
@@ -171,26 +175,26 @@ void state_machine_publish(int status_pub, struct vehicle_status_s *current_stat
|
||||
/*
|
||||
* Private functions, update the state machine
|
||||
*/
|
||||
void state_machine_emergency_always_critical(int status_pub, struct vehicle_status_s *current_status)
|
||||
void state_machine_emergency_always_critical(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
|
||||
{
|
||||
fprintf(stderr, "[commander] EMERGENCY HANDLER\n");
|
||||
/* Depending on the current state go to one of the error states */
|
||||
|
||||
if (current_status->state_machine == SYSTEM_STATE_PREFLIGHT || current_status->state_machine == SYSTEM_STATE_STANDBY || current_status->state_machine == SYSTEM_STATE_GROUND_READY) {
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_GROUND_ERROR);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_ERROR);
|
||||
|
||||
} else if (current_status->state_machine == SYSTEM_STATE_AUTO || current_status->state_machine == SYSTEM_STATE_MANUAL) {
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_MISSION_ABORT);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MISSION_ABORT);
|
||||
|
||||
} else {
|
||||
fprintf(stderr, "[commander] Unknown system state: #%d\n", current_status->state_machine);
|
||||
}
|
||||
}
|
||||
|
||||
void state_machine_emergency(int status_pub, struct vehicle_status_s *current_status) //do not call state_machine_emergency_always_critical if we are in manual mode for these errors
|
||||
void state_machine_emergency(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) //do not call state_machine_emergency_always_critical if we are in manual mode for these errors
|
||||
{
|
||||
if (current_status->state_machine != SYSTEM_STATE_MANUAL) { //if we are in manual: user can react to errors themself
|
||||
state_machine_emergency_always_critical(status_pub, current_status);
|
||||
state_machine_emergency_always_critical(status_pub, current_status, mavlink_fd);
|
||||
|
||||
} else {
|
||||
//global_data_send_mavlink_statustext_message_out("[commander] ERROR: take action immediately! (did not switch to error state because the system is in manual mode)", MAV_SEVERITY_CRITICAL);
|
||||
@@ -399,28 +403,28 @@ void state_machine_emergency(int status_pub, struct vehicle_status_s *current_st
|
||||
/* END SUBSYSTEM/EMERGENCY FUNCTIONS*/
|
||||
|
||||
|
||||
void update_state_machine_got_position_fix(int status_pub, struct vehicle_status_s *current_status)
|
||||
void update_state_machine_got_position_fix(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
|
||||
{
|
||||
/* Depending on the current state switch state */
|
||||
if (current_status->state_machine == SYSTEM_STATE_PREFLIGHT) {
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
|
||||
}
|
||||
}
|
||||
|
||||
void update_state_machine_no_position_fix(int status_pub, struct vehicle_status_s *current_status)
|
||||
void update_state_machine_no_position_fix(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
|
||||
{
|
||||
/* Depending on the current state switch state */
|
||||
if (current_status->state_machine == SYSTEM_STATE_STANDBY || current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_AUTO) {
|
||||
state_machine_emergency(status_pub, current_status);
|
||||
state_machine_emergency(status_pub, current_status, mavlink_fd);
|
||||
}
|
||||
}
|
||||
|
||||
void update_state_machine_arm(int status_pub, struct vehicle_status_s *current_status)
|
||||
void update_state_machine_arm(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
|
||||
{
|
||||
// XXX CHANGE BACK
|
||||
if (current_status->state_machine == SYSTEM_STATE_STANDBY) {
|
||||
printf("[commander] arming\n");
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY);
|
||||
} /*else if (current_status->state_machine == SYSTEM_STATE_AUTO) {
|
||||
|
||||
printf("[commander] landing\n");
|
||||
@@ -428,52 +432,67 @@ void update_state_machine_arm(int status_pub, struct vehicle_status_s *current_s
|
||||
}*/
|
||||
}
|
||||
|
||||
void update_state_machine_disarm(int status_pub, struct vehicle_status_s *current_status)
|
||||
void update_state_machine_disarm(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
|
||||
{
|
||||
if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_PREFLIGHT) {
|
||||
printf("[commander] going standby\n");
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
|
||||
|
||||
} else if (current_status->state_machine == SYSTEM_STATE_STABILIZED || current_status->state_machine == SYSTEM_STATE_AUTO) {
|
||||
printf("[commander] MISSION ABORT!\n");
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
|
||||
}
|
||||
}
|
||||
|
||||
void update_state_machine_mode_manual(int status_pub, struct vehicle_status_s *current_status)
|
||||
void update_state_machine_mode_manual(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
|
||||
{
|
||||
int old_mode = current_status->flight_mode;
|
||||
current_status->flight_mode = VEHICLE_FLIGHT_MODE_MANUAL;
|
||||
current_status->control_manual_enabled = true;
|
||||
if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
|
||||
|
||||
if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_STABILIZED || current_status->state_machine == SYSTEM_STATE_AUTO) {
|
||||
printf("[commander] manual mode\n");
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_MANUAL);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MANUAL);
|
||||
}
|
||||
}
|
||||
|
||||
void update_state_machine_mode_stabilized(int status_pub, struct vehicle_status_s *current_status)
|
||||
void update_state_machine_mode_stabilized(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
|
||||
{
|
||||
int old_mode = current_status->flight_mode;
|
||||
current_status->flight_mode = VEHICLE_FLIGHT_MODE_STABILIZED;
|
||||
current_status->control_manual_enabled = true;
|
||||
if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
|
||||
|
||||
if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_AUTO) {
|
||||
printf("[commander] stabilized mode\n");
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_STABILIZED);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STABILIZED);
|
||||
}
|
||||
}
|
||||
|
||||
void update_state_machine_mode_auto(int status_pub, struct vehicle_status_s *current_status)
|
||||
void update_state_machine_mode_auto(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
|
||||
{
|
||||
int old_mode = current_status->flight_mode;
|
||||
current_status->flight_mode = VEHICLE_FLIGHT_MODE_AUTO;
|
||||
current_status->control_manual_enabled = true;
|
||||
if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
|
||||
|
||||
if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_STABILIZED) {
|
||||
printf("[commander] auto mode\n");
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_AUTO);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_AUTO);
|
||||
}
|
||||
}
|
||||
|
||||
|
||||
uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_s *current_status, uint8_t mode)
|
||||
uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t mode)
|
||||
{
|
||||
printf("in update state request\n");
|
||||
uint8_t ret = 1;
|
||||
|
||||
current_status->mode |= MAV_MODE_FLAG_SAFETY_ARMED;
|
||||
current_status->mode |= VEHICLE_MODE_FLAG_SAFETY_ARMED;
|
||||
/* Set manual input enabled flag */
|
||||
current_status->mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED;
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY);
|
||||
current_status->mode |= VEHICLE_MODE_FLAG_MANUAL_INPUT_ENABLED;
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY);
|
||||
|
||||
/* vehicle is disarmed, mode requests arming */
|
||||
if (!(current_status->mode & VEHICLE_MODE_FLAG_SAFETY_ARMED) && (mode & VEHICLE_MODE_FLAG_SAFETY_ARMED)) {
|
||||
@@ -481,10 +500,10 @@ uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_
|
||||
// XXX REMOVE
|
||||
if (current_status->state_machine == SYSTEM_STATE_STANDBY || current_status->state_machine == SYSTEM_STATE_PREFLIGHT) {
|
||||
/* Set armed flag */
|
||||
current_status->mode |= MAV_MODE_FLAG_SAFETY_ARMED;
|
||||
current_status->mode |= VEHICLE_MODE_FLAG_SAFETY_ARMED;
|
||||
/* Set manual input enabled flag */
|
||||
current_status->mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED;
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY);
|
||||
current_status->mode |= VEHICLE_MODE_FLAG_MANUAL_INPUT_ENABLED;
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY);
|
||||
ret = OK;
|
||||
printf("[commander] arming due to command request\n");
|
||||
}
|
||||
@@ -495,7 +514,7 @@ uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_
|
||||
/* only disarm in ground ready */
|
||||
//if (current_status->state_machine == SYSTEM_STATE_GROUND_READY) {
|
||||
/* Clear armed flag, leave manual input enabled */
|
||||
// current_status->mode &= ~MAV_MODE_FLAG_SAFETY_ARMED;
|
||||
// current_status->mode &= ~VEHICLE_MODE_FLAG_SAFETY_ARMED;
|
||||
// do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
|
||||
// ret = OK;
|
||||
// printf("[commander] disarming due to command request\n");
|
||||
@@ -503,16 +522,16 @@ uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_
|
||||
//}
|
||||
|
||||
/* Switch on HIL if in standby */
|
||||
if ((current_status->state_machine == SYSTEM_STATE_STANDBY) && (mode & MAV_MODE_FLAG_HIL_ENABLED)) {
|
||||
if ((current_status->state_machine == SYSTEM_STATE_STANDBY) && (mode & VEHICLE_MODE_FLAG_HIL_ENABLED)) {
|
||||
/* Enable HIL on request */
|
||||
current_status->mode |= MAV_MODE_FLAG_HIL_ENABLED;
|
||||
current_status->mode |= VEHICLE_MODE_FLAG_HIL_ENABLED;
|
||||
ret = OK;
|
||||
state_machine_publish(status_pub, current_status);
|
||||
state_machine_publish(status_pub, current_status, mavlink_fd);
|
||||
printf("[commander] Enabling HIL\n");
|
||||
}
|
||||
|
||||
/* NEVER actually switch off HIL without reboot */
|
||||
if ((current_status->mode & MAV_MODE_FLAG_HIL_ENABLED) && !(mode & MAV_MODE_FLAG_HIL_ENABLED)) {
|
||||
if ((current_status->mode & VEHICLE_MODE_FLAG_HIL_ENABLED) && !(mode & VEHICLE_MODE_FLAG_HIL_ENABLED)) {
|
||||
fprintf(stderr, "[commander] DENYING request to switch of HIL. Please power cycle (safety reasons)\n");
|
||||
ret = ERROR;
|
||||
}
|
||||
@@ -520,7 +539,7 @@ uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_
|
||||
return ret;
|
||||
}
|
||||
|
||||
uint8_t update_state_machine_custom_mode_request(int status_pub, struct vehicle_status_s *current_status, uint8_t custom_mode) //TODO: add more checks to avoid state switching in critical situations
|
||||
uint8_t update_state_machine_custom_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t custom_mode) //TODO: add more checks to avoid state switching in critical situations
|
||||
{
|
||||
commander_state_machine_t current_system_state = current_status->state_machine;
|
||||
|
||||
@@ -539,7 +558,7 @@ uint8_t update_state_machine_custom_mode_request(int status_pub, struct vehicle_
|
||||
if (current_system_state == SYSTEM_STATE_STANDBY || current_system_state == SYSTEM_STATE_PREFLIGHT) {
|
||||
printf("system will reboot\n");
|
||||
//global_data_send_mavlink_statustext_message_out("Rebooting autopilot.. ", MAV_SEVERITY_INFO);
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_REBOOT);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_REBOOT);
|
||||
ret = 0;
|
||||
}
|
||||
|
||||
@@ -549,7 +568,7 @@ uint8_t update_state_machine_custom_mode_request(int status_pub, struct vehicle_
|
||||
printf("try to switch to auto/takeoff\n");
|
||||
|
||||
if (current_system_state == SYSTEM_STATE_GROUND_READY || current_system_state == SYSTEM_STATE_MANUAL) {
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_AUTO);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_AUTO);
|
||||
printf("state: auto\n");
|
||||
ret = 0;
|
||||
}
|
||||
@@ -560,7 +579,7 @@ uint8_t update_state_machine_custom_mode_request(int status_pub, struct vehicle_
|
||||
printf("try to switch to manual\n");
|
||||
|
||||
if (current_system_state == SYSTEM_STATE_GROUND_READY || current_system_state == SYSTEM_STATE_AUTO) {
|
||||
do_state_update(status_pub, current_status, (commander_state_machine_t)SYSTEM_STATE_MANUAL);
|
||||
do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MANUAL);
|
||||
printf("state: manual\n");
|
||||
ret = 0;
|
||||
}
|
||||
|
||||
@@ -46,8 +46,6 @@
|
||||
|
||||
#include <uORB/uORB.h>
|
||||
#include <uORB/topics/vehicle_status.h>
|
||||
#include <v1.0/common/mavlink.h>
|
||||
|
||||
|
||||
/**
|
||||
* Switch to new state with no checking.
|
||||
@@ -56,8 +54,13 @@
|
||||
* the function does not question the state change, this must be done before
|
||||
* The function performs actions that are connected with the new state (buzzer, reboot, ...)
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*
|
||||
* @return 0 (macro OK) or 1 on error (macro ERROR)
|
||||
*/
|
||||
void do_state_update(int status_pub, struct vehicle_status_s *current_status, commander_state_machine_t new_state);
|
||||
int do_state_update(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, commander_state_machine_t new_state);
|
||||
|
||||
/* These functions decide if an emergency exits and then switch to SYSTEM_STATE_MISSION_ABORT or SYSTEM_STATE_GROUND_ERROR */
|
||||
// void update_state_machine_subsystem_present(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type);
|
||||
@@ -72,43 +75,75 @@ void do_state_update(int status_pub, struct vehicle_status_s *current_status, co
|
||||
|
||||
/**
|
||||
* Handle state machine if got position fix
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
void update_state_machine_got_position_fix(int status_pub, struct vehicle_status_s *current_status);
|
||||
void update_state_machine_got_position_fix(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd);
|
||||
|
||||
/**
|
||||
* Handle state machine if position fix lost
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
void update_state_machine_no_position_fix(int status_pub, struct vehicle_status_s *current_status);
|
||||
void update_state_machine_no_position_fix(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd);
|
||||
|
||||
/**
|
||||
* Handle state machine if user wants to arm
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
void update_state_machine_arm(int status_pub, struct vehicle_status_s *current_status);
|
||||
void update_state_machine_arm(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd);
|
||||
|
||||
/**
|
||||
* Handle state machine if user wants to disarm
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
void update_state_machine_disarm(int status_pub, struct vehicle_status_s *current_status);
|
||||
void update_state_machine_disarm(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd);
|
||||
|
||||
/**
|
||||
* Handle state machine if mode switch is manual
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
void update_state_machine_mode_manual(int status_pub, struct vehicle_status_s *current_status);
|
||||
void update_state_machine_mode_manual(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd);
|
||||
|
||||
/**
|
||||
* Handle state machine if mode switch is stabilized
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
void update_state_machine_mode_stabilized(int status_pub, struct vehicle_status_s *current_status);
|
||||
void update_state_machine_mode_stabilized(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd);
|
||||
|
||||
/**
|
||||
* Handle state machine if mode switch is auto
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
void update_state_machine_mode_auto(int status_pub, struct vehicle_status_s *current_status);
|
||||
void update_state_machine_mode_auto(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd);
|
||||
|
||||
/**
|
||||
* Publish current state information
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
void state_machine_publish(int status_pub, struct vehicle_status_s *current_status);
|
||||
void state_machine_publish(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd);
|
||||
|
||||
|
||||
/*
|
||||
@@ -119,17 +154,39 @@ void state_machine_publish(int status_pub, struct vehicle_status_s *current_stat
|
||||
|
||||
/**
|
||||
* Handles *incoming request* to switch to a specific state, if state change is successful returns 0
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_s *current_status, uint8_t mode);
|
||||
uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t mode);
|
||||
|
||||
/**
|
||||
* Handles *incoming request* to switch to a specific custom state, if state change is successful returns 0
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
uint8_t update_state_machine_custom_mode_request(int status_pub, struct vehicle_status_s *current_status, uint8_t custom_mode);
|
||||
uint8_t update_state_machine_custom_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t custom_mode);
|
||||
|
||||
/**
|
||||
* Always switches to critical mode under any circumstances.
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
void state_machine_emergency_always_critical(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd);
|
||||
|
||||
void state_machine_emergency_always_critical(int status_pub, struct vehicle_status_s *current_status);
|
||||
void state_machine_emergency(int status_pub, struct vehicle_status_s *current_status);
|
||||
/**
|
||||
* Switches to emergency if required.
|
||||
*
|
||||
* @param status_pub file descriptor for state update topic publication
|
||||
* @param current_status pointer to the current state machine to operate on
|
||||
* @param mavlink_fd file descriptor for MAVLink statustext messages
|
||||
*/
|
||||
void state_machine_emergency(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd);
|
||||
|
||||
|
||||
|
||||
|
||||
Reference in New Issue
Block a user