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Improved command handling, added a low priority task and various fixes

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This commit is contained in:
Julian Oes
2013-03-25 14:53:54 -07:00
parent b1e2011fcc
commit 3665d7b86f
2 changed files with 312 additions and 312 deletions
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apps/commander/commander.c
+296 -312
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@@ -143,16 +143,26 @@ static int daemon_task; /**< Handle of daemon task / thread */
static struct vehicle_status_s current_status;
static orb_advert_t stat_pub;
/* XXX ? */
// static uint16_t nofix_counter = 0;
// static uint16_t gotfix_counter = 0;
/* XXX ? */
/* timout until lowlevel failsafe */
static unsigned int failsafe_lowlevel_timeout_ms;
/* tasks waiting for low prio thread */
enum {
LOW_PRIO_TASK_NONE = 0,
LOW_PRIO_TASK_PARAM_SAVE,
LOW_PRIO_TASK_PARAM_LOAD,
LOW_PRIO_TASK_GYRO_CALIBRATION,
LOW_PRIO_TASK_MAG_CALIBRATION,
LOW_PRIO_TASK_ALTITUDE_CALIBRATION,
LOW_PRIO_TASK_RC_CALIBRATION,
LOW_PRIO_TASK_ACCEL_CALIBRATION,
LOW_PRIO_TASK_AIRSPEED_CALIBRATION
} low_prio_task;
/* pthread loops */
static void *orb_receive_loop(void *arg);
static void *commander_low_prio_loop(void *arg);
__EXPORT int commander_main(int argc, char *argv[]);
@@ -161,18 +171,23 @@ __EXPORT int commander_main(int argc, char *argv[]);
*/
int commander_thread_main(int argc, char *argv[]);
static int buzzer_init(void);
static void buzzer_deinit(void);
static int led_init(void);
static void led_deinit(void);
static int led_toggle(int led);
static int led_on(int led);
static int led_off(int led);
static void do_gyro_calibration(int status_pub, struct vehicle_status_s *status);
static void do_mag_calibration(int status_pub, struct vehicle_status_s *status);
static void do_rc_calibration(int status_pub, struct vehicle_status_s *status);
static void do_accel_calibration(int status_pub, struct vehicle_status_s *status);
static void do_airspeed_calibration(int status_pub, struct vehicle_status_s *status);
int buzzer_init(void);
void buzzer_deinit(void);
int led_init(void);
void led_deinit(void);
int led_toggle(int led);
int led_on(int led);
int led_off(int led);
void tune_error(void);
void tune_positive(void);
void tune_neutral(void);
void tune_negative(void);
void do_reboot(void);
void do_gyro_calibration(void);
void do_mag_calibration(void);
void do_rc_calibration(void);
void do_accel_calibration(void);
void do_airspeed_calibration(void);
static void handle_command(int status_pub, struct vehicle_status_s *current_status, struct vehicle_command_s *cmd);
@@ -184,7 +199,7 @@ int trigger_audio_alarm(uint8_t old_mode, uint8_t old_state, uint8_t new_mode, u
/**
* Print the correct usage.
*/
static void usage(const char *reason);
void usage(const char *reason);
/**
* Sort calibration values.
@@ -196,7 +211,7 @@ static void usage(const char *reason);
*/
// static void cal_bsort(float a[], int n);
static int buzzer_init()
int buzzer_init()
{
buzzer = open("/dev/tone_alarm", O_WRONLY);
@@ -208,13 +223,13 @@ static int buzzer_init()
return 0;
}
static void buzzer_deinit()
void buzzer_deinit()
{
close(buzzer);
}
static int led_init()
int led_init()
{
leds = open(LED_DEVICE_PATH, 0);
@@ -231,12 +246,12 @@ static int led_init()
return 0;
}
static void led_deinit()
void led_deinit()
{
close(leds);
}
static int led_toggle(int led)
int led_toggle(int led)
{
static int last_blue = LED_ON;
static int last_amber = LED_ON;
@@ -248,59 +263,50 @@ static int led_toggle(int led)
return ioctl(leds, ((led == LED_BLUE) ? last_blue : last_amber), led);
}
static int led_on(int led)
int led_on(int led)
{
return ioctl(leds, LED_ON, led);
}
static int led_off(int led)
int led_off(int led)
{
return ioctl(leds, LED_OFF, led);
}
enum AUDIO_PATTERN {
AUDIO_PATTERN_ERROR = 2,
AUDIO_PATTERN_NOTIFY_POSITIVE = 3,
AUDIO_PATTERN_NOTIFY_NEUTRAL = 4,
AUDIO_PATTERN_NOTIFY_NEGATIVE = 5,
AUDIO_PATTERN_NOTIFY_CHARGE = 6
};
int trigger_audio_alarm(uint8_t old_mode, uint8_t old_state, uint8_t new_mode, uint8_t new_state)
void tune_error()
{
#warning add alarms for state transitions
/* Trigger alarm if going into any error state */
// if (((new_state == SYSTEM_STATE_GROUND_ERROR) && (old_state != SYSTEM_STATE_GROUND_ERROR)) ||
// ((new_state == SYSTEM_STATE_MISSION_ABORT) && (old_state != SYSTEM_STATE_MISSION_ABORT))) {
// ioctl(buzzer, TONE_SET_ALARM, 0);
// ioctl(buzzer, TONE_SET_ALARM, AUDIO_PATTERN_ERROR);
// }
/* Trigger neutral on arming / disarming */
// if (((new_state == SYSTEM_STATE_GROUND_READY) && (old_state != SYSTEM_STATE_GROUND_READY))) {
// ioctl(buzzer, TONE_SET_ALARM, 0);
// ioctl(buzzer, TONE_SET_ALARM, AUDIO_PATTERN_NOTIFY_NEUTRAL);
// }
/* Trigger Tetris on being bored */
return 0;
ioctl(buzzer, TONE_SET_ALARM, 2);
}
void tune_confirm(void)
void tune_positive()
{
ioctl(buzzer, TONE_SET_ALARM, 3);
}
void tune_error(void)
void tune_neutral()
{
/* XXX change alarm to 2 tones*/
ioctl(buzzer, TONE_SET_ALARM, 4);
}
void do_rc_calibration(int status_pub, struct vehicle_status_s *status)
void tune_negative()
{
ioctl(buzzer, TONE_SET_ALARM, 5);
}
void do_reboot()
{
mavlink_log_critical(mavlink_fd, "REBOOTING SYSTEM");
usleep(500000);
up_systemreset();
/* SPECIAL CASE: NEVER RETURNS FROM THIS FUNCTION CALL */
}
void do_rc_calibration()
{
mavlink_log_info(mavlink_fd, "trim calibration starting");
if (current_status.offboard_control_signal_lost) {
mavlink_log_critical(mavlink_fd, "TRIM CAL: ABORT. No RC signal.");
return;
@@ -311,7 +317,6 @@ void do_rc_calibration(int status_pub, struct vehicle_status_s *status)
orb_copy(ORB_ID(manual_control_setpoint), sub_man, &sp);
/* set parameters */
float p = sp.roll;
param_set(param_find("TRIM_ROLL"), &p);
p = sp.pitch;
@@ -320,22 +325,21 @@ void do_rc_calibration(int status_pub, struct vehicle_status_s *status)
param_set(param_find("TRIM_YAW"), &p);
/* store to permanent storage */
/* auto-save to EEPROM */
/* auto-save */
int save_ret = param_save_default();
if (save_ret != 0) {
mavlink_log_critical(mavlink_fd, "TRIM CAL: WARN: auto-save of params failed");
}
tune_positive();
mavlink_log_info(mavlink_fd, "trim calibration done");
}
void do_mag_calibration(int status_pub, struct vehicle_status_s *status)
void do_mag_calibration()
{
/* set to mag calibration mode */
// status->flag_preflight_mag_calibration = true;
// state_machine_publish(status_pub, status, mavlink_fd);
mavlink_log_info(mavlink_fd, "mag calibration starting, hold still");
int sub_mag = orb_subscribe(ORB_ID(sensor_mag));
struct mag_report mag;
@@ -350,15 +354,6 @@ void do_mag_calibration(int status_pub, struct vehicle_status_s *status)
/* limit update rate to get equally spaced measurements over time (in ms) */
orb_set_interval(sub_mag, (calibration_interval / 1000) / calibration_maxcount);
// XXX old cal
// * FLT_MIN is not the most negative float number,
// * but the smallest number by magnitude float can
// * represent. Use -FLT_MAX to initialize the most
// * negative number
// float mag_max[3] = {-FLT_MAX, -FLT_MAX, -FLT_MAX};
// float mag_min[3] = {FLT_MAX, FLT_MAX, FLT_MAX};
int fd = open(MAG_DEVICE_PATH, O_RDONLY);
/* erase old calibration */
@@ -404,10 +399,6 @@ void do_mag_calibration(int status_pub, struct vehicle_status_s *status)
return;
}
tune_confirm();
sleep(2);
tune_confirm();
while (hrt_absolute_time() < calibration_deadline &&
calibration_counter < calibration_maxcount) {
@@ -421,9 +412,9 @@ void do_mag_calibration(int status_pub, struct vehicle_status_s *status)
axis_index++;
char buf[50];
sprintf(buf, "Please rotate around %c", axislabels[axis_index]);
sprintf(buf, "please rotate around %c", axislabels[axis_index]);
mavlink_log_info(mavlink_fd, buf);
tune_confirm();
tune_neutral();
axis_deadline += calibration_interval / 3;
}
@@ -559,28 +550,19 @@ void do_mag_calibration(int status_pub, struct vehicle_status_s *status)
mavlink_log_info(mavlink_fd, "mag calibration done");
tune_confirm();
sleep(2);
tune_confirm();
sleep(2);
tune_positive();
/* third beep by cal end routine */
} else {
mavlink_log_info(mavlink_fd, "mag calibration FAILED (NaN in sphere fit)");
}
/* disable calibration mode */
// status->flag_preflight_mag_calibration = false;
// state_machine_publish(status_pub, status, mavlink_fd);
close(sub_mag);
}
void do_gyro_calibration(int status_pub, struct vehicle_status_s *status)
void do_gyro_calibration()
{
/* set to gyro calibration mode */
// status->flag_preflight_gyro_calibration = true;
// state_machine_publish(status_pub, status, mavlink_fd);
mavlink_log_info(mavlink_fd, "gyro calibration starting, hold still");
const int calibration_count = 5000;
@@ -631,10 +613,6 @@ void do_gyro_calibration(int status_pub, struct vehicle_status_s *status)
gyro_offset[1] = gyro_offset[1] / calibration_count;
gyro_offset[2] = gyro_offset[2] / calibration_count;
/* exit gyro calibration mode */
// status->flag_preflight_gyro_calibration = false;
// state_machine_publish(status_pub, status, mavlink_fd);
if (isfinite(gyro_offset[0]) && isfinite(gyro_offset[1]) && isfinite(gyro_offset[2])) {
if (param_set(param_find("SENS_GYRO_XOFF"), &(gyro_offset[0]))
@@ -671,10 +649,7 @@ void do_gyro_calibration(int status_pub, struct vehicle_status_s *status)
// mavlink_log_info(mavlink_fd, buf);
mavlink_log_info(mavlink_fd, "gyro calibration done");
tune_confirm();
sleep(2);
tune_confirm();
sleep(2);
tune_positive();
/* third beep by cal end routine */
} else {
@@ -684,14 +659,10 @@ void do_gyro_calibration(int status_pub, struct vehicle_status_s *status)
close(sub_sensor_combined);
}
void do_accel_calibration(int status_pub, struct vehicle_status_s *status)
void do_accel_calibration()
{
/* announce change */
mavlink_log_info(mavlink_fd, "keep it level and still");
/* set to accel calibration mode */
// status->flag_preflight_accel_calibration = true;
// state_machine_publish(status_pub, status, mavlink_fd);
/* give directions */
mavlink_log_info(mavlink_fd, "accel calibration starting, keep it level");
const int calibration_count = 2500;
@@ -787,28 +758,19 @@ void do_accel_calibration(int status_pub, struct vehicle_status_s *status)
//mavlink_log_info(mavlink_fd, buf);
mavlink_log_info(mavlink_fd, "accel calibration done");
tune_confirm();
sleep(2);
tune_confirm();
sleep(2);
/* third beep by cal end routine */
tune_positive();
} else {
mavlink_log_info(mavlink_fd, "accel calibration FAILED (NaN)");
}
/* exit accel calibration mode */
// status->flag_preflight_accel_calibration = false;
// state_machine_publish(status_pub, status, mavlink_fd);
close(sub_sensor_combined);
}
static void do_airspeed_calibration(int status_pub, struct vehicle_status_s *status)
void do_airspeed_calibration()
{
/* announce change */
mavlink_log_info(mavlink_fd, "keep it still");
/* give directions */
mavlink_log_info(mavlink_fd, "airspeed calibration starting, keep it still");
const int calibration_count = 2500;
@@ -857,11 +819,7 @@ static void do_airspeed_calibration(int status_pub, struct vehicle_status_s *sta
//mavlink_log_info(mavlink_fd, buf);
mavlink_log_info(mavlink_fd, "airspeed calibration done");
tune_confirm();
sleep(2);
tune_confirm();
sleep(2);
/* third beep by cal end routine */
tune_positive();
} else {
mavlink_log_info(mavlink_fd, "airspeed calibration FAILED (NaN)");
@@ -870,16 +828,11 @@ static void do_airspeed_calibration(int status_pub, struct vehicle_status_s *sta
close(sub_differential_pressure);
}
void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_status, struct vehicle_command_s *cmd)
{
/* result of the command */
uint8_t result = VEHICLE_CMD_RESULT_UNSUPPORTED;
/* announce command handling */
tune_confirm();
/* request to set different system mode */
switch (cmd->command) {
case VEHICLE_CMD_DO_SET_MODE:
@@ -935,12 +888,16 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
/* request for an autopilot reboot */
if ((int)cmd->param1 == 1) {
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_REBOOT, mavlink_fd)) {
/* SPECIAL CASE: SYSTEM WILL NEVER RETURN HERE */
/* reboot is executed later, after positive tune is sent */
result = VEHICLE_CMD_RESULT_ACCEPTED;
tune_positive();
/* SPECIAL CASE: SYSTEM WILL NEVER RETURN HERE */
do_reboot();
} else {
/* system may return here */
result = VEHICLE_CMD_RESULT_DENIED;
tune_negative();
}
}
}
@@ -971,234 +928,155 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
//
/* preflight calibration */
case VEHICLE_CMD_PREFLIGHT_CALIBRATION: {
bool handled = false;
/* gyro calibration */
if ((int)(cmd->param1) == 1) {
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, mavlink_fd)) {
result = VEHICLE_CMD_RESULT_ACCEPTED;
mavlink_log_info(mavlink_fd, "starting gyro cal");
tune_confirm();
do_gyro_calibration(status_pub, &current_status);
mavlink_log_info(mavlink_fd, "finished gyro cal");
tune_confirm();
// XXX if this fails, go to ERROR
arming_state_transition(status_pub, &current_status, ARMING_STATE_STANDBY, mavlink_fd);
/* check if no other task is scheduled */
if(low_prio_task == LOW_PRIO_TASK_NONE) {
/* try to go to INIT/PREFLIGHT arming state */
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, mavlink_fd)) {
result = VEHICLE_CMD_RESULT_ACCEPTED;
/* now set the task for the low prio thread */
low_prio_task = LOW_PRIO_TASK_GYRO_CALIBRATION;
} else {
result = VEHICLE_CMD_RESULT_DENIED;
}
} else {
result = VEHICLE_CMD_RESULT_DENIED;
result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
}
handled = true;
}
/* magnetometer calibration */
if ((int)(cmd->param2) == 1) {
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, mavlink_fd)) {
result = VEHICLE_CMD_RESULT_ACCEPTED;
mavlink_log_info(mavlink_fd, "starting mag cal");
tune_confirm();
do_mag_calibration(status_pub, &current_status);
mavlink_log_info(mavlink_fd, "finished mag cal");
tune_confirm();
// XXX if this fails, go to ERROR
arming_state_transition(status_pub, &current_status, ARMING_STATE_STANDBY, mavlink_fd);
/* check if no other task is scheduled */
if(low_prio_task == LOW_PRIO_TASK_NONE) {
/* try to go to INIT/PREFLIGHT arming state */
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, mavlink_fd)) {
result = VEHICLE_CMD_RESULT_ACCEPTED;
/* now set the task for the low prio thread */
low_prio_task = LOW_PRIO_TASK_MAG_CALIBRATION;
} else {
result = VEHICLE_CMD_RESULT_DENIED;
}
} else {
result = VEHICLE_CMD_RESULT_DENIED;
result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
}
handled = true;
}
#if 0
/* zero-altitude pressure calibration */
if ((int)(cmd->param3) == 1) {
/* transition to calibration state */
// XXX add this again
// if (OK == do_arming_state_update(status_pub, &current_status, mavlink_fd, ARMING_STATE_INIT)
// && OK == do_navigation_state_update(status_pub, &current_status, mavlink_fd, NAVIGATION_STATE_INIT)) {
//
// // XXX implement this
// mavlink_log_info(mavlink_fd, "zero altitude cal. not implemented");
// tune_confirm();
//
// /* back to standby state */
// do_arming_state_update(status_pub, &current_status, mavlink_fd, ARMING_STATE_STANDBY);
// do_navigation_state_update(status_pub, &current_status, mavlink_fd, NAVIGATION_STATE_STANDBY);
//
// } else {
// mavlink_log_critical(mavlink_fd, "REJECTING altitude calibration");
// result = VEHICLE_CMD_RESULT_DENIED;
// }
handled = true;
/* check if no other task is scheduled */
if(low_prio_task == LOW_PRIO_TASK_NONE) {
/* try to go to INIT/PREFLIGHT arming state */
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, mavlink_fd)) {
result = VEHICLE_CMD_RESULT_ACCEPTED;
/* now set the task for the low prio thread */
low_prio_task = LOW_PRIO_TASK_ALTITUDE_CALIBRATION;
} else {
result = VEHICLE_CMD_RESULT_DENIED;
}
} else {
result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
}
}
#endif
#if 0
/* trim calibration */
if ((int)(cmd->param4) == 1) {
/* transition to calibration state */
// XXX add this again
// if (OK == do_arming_state_update(status_pub, &current_status, mavlink_fd, ARMING_STATE_INIT)
// && OK == do_navigation_state_update(status_pub, &current_status, mavlink_fd, NAVIGATION_STATE_INIT)) {
// mavlink_log_info(mavlink_fd, "starting trim cal");
// tune_confirm();
// do_rc_calibration(status_pub, &current_status);
// mavlink_log_info(mavlink_fd, "finished trim cal");
// tune_confirm();
//
// /* back to standby state */
// do_arming_state_update(status_pub, &current_status, mavlink_fd, ARMING_STATE_STANDBY);
// do_navigation_state_update(status_pub, &current_status, mavlink_fd, NAVIGATION_STATE_STANDBY);
//
// result = VEHICLE_CMD_RESULT_ACCEPTED;
//
// } else {
// mavlink_log_critical(mavlink_fd, "REJECTING trim cal");
// result = VEHICLE_CMD_RESULT_DENIED;
// }
handled = true;
/* check if no other task is scheduled */
if(low_prio_task == LOW_PRIO_TASK_NONE) {
/* try to go to INIT/PREFLIGHT arming state */
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, mavlink_fd)) {
result = VEHICLE_CMD_RESULT_ACCEPTED;
/* now set the task for the low prio thread */
low_prio_task = LOW_PRIO_TASK_RC_CALIBRATION;
} else {
result = VEHICLE_CMD_RESULT_DENIED;
}
} else {
result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
}
}
#endif
/* accel calibration */
if ((int)(cmd->param5) == 1) {
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, mavlink_fd)) {
result = VEHICLE_CMD_RESULT_ACCEPTED;
mavlink_log_info(mavlink_fd, "starting acc cal");
tune_confirm();
do_accel_calibration(status_pub, &current_status);
mavlink_log_info(mavlink_fd, "finished acc cal");
tune_confirm();
// XXX what if this fails
arming_state_transition(status_pub, &current_status, ARMING_STATE_STANDBY, mavlink_fd);
/* check if no other task is scheduled */
if(low_prio_task == LOW_PRIO_TASK_NONE) {
/* try to go to INIT/PREFLIGHT arming state */
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, mavlink_fd)) {
result = VEHICLE_CMD_RESULT_ACCEPTED;
/* now set the task for the low prio thread */
low_prio_task = LOW_PRIO_TASK_ACCEL_CALIBRATION;
} else {
result = VEHICLE_CMD_RESULT_DENIED;
}
} else {
result = VEHICLE_CMD_RESULT_DENIED;
result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
}
handled = true;
}
/* airspeed calibration */
if ((int)(cmd->param6) == 1) {
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, mavlink_fd)) {
result = VEHICLE_CMD_RESULT_ACCEPTED;
mavlink_log_info(mavlink_fd, "starting airspeed cal");
tune_confirm();
do_airspeed_calibration(status_pub, &current_status);
mavlink_log_info(mavlink_fd, "finished airspeed cal");
tune_confirm();
// XXX if this fails, go to ERROR
arming_state_transition(status_pub, &current_status, ARMING_STATE_STANDBY, mavlink_fd);
/* check if no other task is scheduled */
if(low_prio_task == LOW_PRIO_TASK_NONE) {
/* try to go to INIT/PREFLIGHT arming state */
if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, mavlink_fd)) {
result = VEHICLE_CMD_RESULT_ACCEPTED;
/* now set the task for the low prio thread */
low_prio_task = LOW_PRIO_TASK_AIRSPEED_CALIBRATION;
} else {
result = VEHICLE_CMD_RESULT_DENIED;
}
} else {
result = VEHICLE_CMD_RESULT_DENIED;
result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
}
handled = true;
}
/* none found */
if (!handled) {
//warnx("refusing unsupported calibration request\n");
mavlink_log_critical(mavlink_fd, "CMD refusing unsup. calib. request");
result = VEHICLE_CMD_RESULT_UNSUPPORTED;
}
}
break;
case VEHICLE_CMD_PREFLIGHT_STORAGE: {
if (current_status.flag_fmu_armed &&
((current_status.system_type == VEHICLE_TYPE_QUADROTOR) ||
(current_status.system_type == VEHICLE_TYPE_HEXAROTOR) ||
(current_status.system_type == VEHICLE_TYPE_OCTOROTOR))) {
/* do not perform expensive memory tasks on multirotors in flight */
// XXX this is over-safe, as soon as cmd is in low prio thread this can be allowed
mavlink_log_info(mavlink_fd, "REJECTING save cmd while multicopter armed");
if (((int)(cmd->param1)) == 0) {
/* check if no other task is scheduled */
if(low_prio_task == LOW_PRIO_TASK_NONE) {
low_prio_task = LOW_PRIO_TASK_PARAM_LOAD;
result = VEHICLE_CMD_RESULT_ACCEPTED;
} else {
result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
}
// XXX move this to LOW PRIO THREAD of commander app
/* Read all parameters from EEPROM to RAM */
if (((int)(cmd->param1)) == 0) {
} else if (((int)(cmd->param1)) == 1) {
/* read all parameters from EEPROM to RAM */
int read_ret = param_load_default();
if (read_ret == OK) {
//warnx("[mavlink pm] Loaded EEPROM params in RAM\n");
mavlink_log_info(mavlink_fd, "OK loading params from");
mavlink_log_info(mavlink_fd, param_get_default_file());
result = VEHICLE_CMD_RESULT_ACCEPTED;
} else if (read_ret == 1) {
mavlink_log_info(mavlink_fd, "OK no changes in");
mavlink_log_info(mavlink_fd, param_get_default_file());
result = VEHICLE_CMD_RESULT_ACCEPTED;
} else {
if (read_ret < -1) {
mavlink_log_info(mavlink_fd, "ERR loading params from");
mavlink_log_info(mavlink_fd, param_get_default_file());
} else {
mavlink_log_info(mavlink_fd, "ERR no param file named");
mavlink_log_info(mavlink_fd, param_get_default_file());
}
result = VEHICLE_CMD_RESULT_FAILED;
}
} else if (((int)(cmd->param1)) == 1) {
/* write all parameters from RAM to EEPROM */
int write_ret = param_save_default();
if (write_ret == OK) {
mavlink_log_info(mavlink_fd, "OK saved param file");
mavlink_log_info(mavlink_fd, param_get_default_file());
result = VEHICLE_CMD_RESULT_ACCEPTED;
} else {
if (write_ret < -1) {
mavlink_log_info(mavlink_fd, "ERR params file does not exit:");
mavlink_log_info(mavlink_fd, param_get_default_file());
} else {
mavlink_log_info(mavlink_fd, "ERR writing params to");
mavlink_log_info(mavlink_fd, param_get_default_file());
}
result = VEHICLE_CMD_RESULT_FAILED;
}
} else {
mavlink_log_info(mavlink_fd, "[pm] refusing unsupp. STOR request");
result = VEHICLE_CMD_RESULT_UNSUPPORTED;
}
/* check if no other task is scheduled */
if(low_prio_task == LOW_PRIO_TASK_NONE) {
low_prio_task = LOW_PRIO_TASK_PARAM_LOAD;
result = VEHICLE_CMD_RESULT_ACCEPTED;
} else {
result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
}
}
break;
} break;
default: {
mavlink_log_critical(mavlink_fd, "[cmd] refusing unsupported command");
result = VEHICLE_CMD_RESULT_UNSUPPORTED;
/* announce command rejection */
ioctl(buzzer, TONE_SET_ALARM, 4);
}
break;
}
@@ -1207,10 +1085,12 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta
if (result == VEHICLE_CMD_RESULT_FAILED ||
result == VEHICLE_CMD_RESULT_DENIED ||
result == VEHICLE_CMD_RESULT_UNSUPPORTED) {
ioctl(buzzer, TONE_SET_ALARM, 5);
tune_negative();
} else if (result == VEHICLE_CMD_RESULT_ACCEPTED) {
tune_confirm();
tune_positive();
}
/* send any requested ACKs */
@@ -1324,8 +1204,7 @@ float battery_remaining_estimate_voltage(float voltage)
return ret;
}
static void
usage(const char *reason)
void usage(const char *reason)
{
if (reason)
fprintf(stderr, "%s\n", reason);
@@ -1405,6 +1284,7 @@ int commander_thread_main(int argc, char *argv[])
/* pthreads for command and subsystem info handling */
// pthread_t command_handling_thread;
pthread_t subsystem_info_thread;
pthread_t commander_low_prio_thread;
/* initialize */
if (led_init() != 0) {
@@ -1477,6 +1357,16 @@ int commander_thread_main(int argc, char *argv[])
pthread_attr_setstacksize(&subsystem_info_attr, 2048);
pthread_create(&subsystem_info_thread, &subsystem_info_attr, orb_receive_loop, &current_status);
pthread_attr_t commander_low_prio_attr;
pthread_attr_init(&commander_low_prio_attr);
pthread_attr_setstacksize(&commander_low_prio_attr, 2048);
struct sched_param param;
/* low priority */
param.sched_priority = SCHED_PRIORITY_DEFAULT - 50;
(void)pthread_attr_setschedparam(&commander_low_prio_attr, &param);
pthread_create(&commander_low_prio_thread, &commander_low_prio_attr, commander_low_prio_loop, NULL);
/* Start monitoring loop */
uint16_t counter = 0;
@@ -1487,12 +1377,14 @@ int commander_thread_main(int argc, char *argv[])
bool critical_battery_voltage_actions_done = false;
uint8_t low_voltage_counter = 0;
uint16_t critical_voltage_counter = 0;
int16_t mode_switch_rc_value;
float bat_remain = 1.0f;
uint16_t stick_off_counter = 0;
uint16_t stick_on_counter = 0;
/* XXX what exactly is this for? */
uint64_t last_print_time = 0;
/* Subscribe to manual control data */
int sp_man_sub = orb_subscribe(ORB_ID(manual_control_setpoint));
struct manual_control_setpoint_s sp_man;
@@ -1562,7 +1454,9 @@ int commander_thread_main(int argc, char *argv[])
thread_running = true;
uint64_t start_time = hrt_absolute_time();
uint64_t failsave_ll_start_time = 0;
/* XXX use this! */
//uint64_t failsave_ll_start_time = 0;
bool state_changed = true;
bool param_init_forced = true;
@@ -1727,7 +1621,7 @@ int commander_thread_main(int argc, char *argv[])
} else if (bat_remain < 0.2f && battery_voltage_valid && (counter % ((1000000 / COMMANDER_MONITORING_INTERVAL) / 2) == 0)) {
/* For less than 20%, start be slightly annoying at 1 Hz */
ioctl(buzzer, TONE_SET_ALARM, 0);
tune_confirm();
tune_positive();
} else if (bat_remain < 0.2f && battery_voltage_valid && (counter % ((1000000 / COMMANDER_MONITORING_INTERVAL) / 2) == 2)) {
ioctl(buzzer, TONE_SET_ALARM, 0);
@@ -1916,7 +1810,7 @@ int commander_thread_main(int argc, char *argv[])
/* mark home position as set */
home_position_set = true;
tune_confirm();
tune_positive();
}
}
@@ -2206,13 +2100,19 @@ int commander_thread_main(int argc, char *argv[])
current_status.rc_signal_lost_interval = 0;
} else {
static uint64_t last_print_time = 0;
/* print error message for first RC glitch and then every 5 s / 5000 ms) */
if (!current_status.rc_signal_cutting_off || ((hrt_absolute_time() - last_print_time) > 5000000)) {
/* only complain if the offboard control is NOT active */
current_status.rc_signal_cutting_off = true;
mavlink_log_critical(mavlink_fd, "CRITICAL - NO REMOTE SIGNAL!");
if (!current_status.rc_signal_cutting_off) {
printf("Reason: not rc_signal_cutting_off\n");
} else {
printf("last print time: %llu\n", last_print_time);
}
last_print_time = hrt_absolute_time();
}
@@ -2270,7 +2170,7 @@ int commander_thread_main(int argc, char *argv[])
current_status.flag_control_manual_enabled = false;
current_status.flag_control_offboard_enabled = true;
state_changed = true;
tune_confirm();
tune_positive();
mavlink_log_critical(mavlink_fd, "DETECTED OFFBOARD SIGNAL FIRST");
@@ -2278,7 +2178,7 @@ int commander_thread_main(int argc, char *argv[])
if (current_status.offboard_control_signal_lost) {
mavlink_log_critical(mavlink_fd, "RECOVERY OFFBOARD CONTROL");
state_changed = true;
tune_confirm();
tune_positive();
}
}
@@ -2298,7 +2198,6 @@ int commander_thread_main(int argc, char *argv[])
}
} else {
static uint64_t last_print_time = 0;
/* print error message for first RC glitch and then every 5 s / 5000 ms) */
if (!current_status.offboard_control_signal_weak || ((hrt_absolute_time() - last_print_time) > 5000000)) {
@@ -2314,7 +2213,7 @@ int commander_thread_main(int argc, char *argv[])
if (current_status.offboard_control_signal_lost_interval > 100000) {
current_status.offboard_control_signal_lost = true;
current_status.failsave_lowlevel_start_time = hrt_absolute_time();
tune_confirm();
tune_positive();
/* kill motors after timeout */
if (hrt_absolute_time() - current_status.failsave_lowlevel_start_time > failsafe_lowlevel_timeout_ms * 1000) {
@@ -2352,6 +2251,7 @@ int commander_thread_main(int argc, char *argv[])
/* Store old modes to detect and act on state transitions */
voltage_previous = current_status.voltage_battery;
/* XXX use this voltage_previous */
fflush(stdout);
counter++;
usleep(COMMANDER_MONITORING_INTERVAL);
@@ -2360,6 +2260,7 @@ int commander_thread_main(int argc, char *argv[])
/* wait for threads to complete */
// pthread_join(command_handling_thread, NULL);
pthread_join(subsystem_info_thread, NULL);
pthread_join(commander_low_prio_thread, NULL);
/* close fds */
led_deinit();
@@ -2377,3 +2278,86 @@ int commander_thread_main(int argc, char *argv[])
return 0;
}
static void *commander_low_prio_loop(void *arg)
{
/* Set thread name */
prctl(PR_SET_NAME, "commander low prio", getpid());
while (!thread_should_exit) {
switch (low_prio_task) {
case LOW_PRIO_TASK_PARAM_LOAD:
if (0 == param_load_default()) {
mavlink_log_info(mavlink_fd, "Param load success");
} else {
mavlink_log_critical(mavlink_fd, "Param load ERROR");
tune_error();
}
low_prio_task = LOW_PRIO_TASK_NONE;
break;
case LOW_PRIO_TASK_PARAM_SAVE:
if (0 == param_save_default()) {
mavlink_log_info(mavlink_fd, "Param save success");
} else {
mavlink_log_critical(mavlink_fd, "Param save ERROR");
tune_error();
}
low_prio_task = LOW_PRIO_TASK_NONE;
break;
case LOW_PRIO_TASK_GYRO_CALIBRATION:
do_gyro_calibration();
low_prio_task = LOW_PRIO_TASK_NONE;
break;
case LOW_PRIO_TASK_MAG_CALIBRATION:
do_mag_calibration();
low_prio_task = LOW_PRIO_TASK_NONE;
break;
case LOW_PRIO_TASK_ALTITUDE_CALIBRATION:
// do_baro_calibration();
case LOW_PRIO_TASK_RC_CALIBRATION:
// do_rc_calibration();
low_prio_task = LOW_PRIO_TASK_NONE;
break;
case LOW_PRIO_TASK_ACCEL_CALIBRATION:
do_accel_calibration();
low_prio_task = LOW_PRIO_TASK_NONE;
break;
case LOW_PRIO_TASK_AIRSPEED_CALIBRATION:
do_airspeed_calibration();
low_prio_task = LOW_PRIO_TASK_NONE;
break;
case LOW_PRIO_TASK_NONE:
default:
/* slow down to 10Hz */
usleep(100000);
break;
}
}
return 0;
}
apps/commander/state_machine_helper.c
+16
View File
@@ -117,6 +117,22 @@ int arming_state_transition(int status_pub, struct vehicle_status_s *current_sta
current_state->flag_fmu_armed = false;
}
break;
case ARMING_STATE_REBOOT:
/* an armed error happens when ARMED obviously */
if (current_state->arming_state == ARMING_STATE_INIT
|| current_state->arming_state == ARMING_STATE_STANDBY
|| current_state->arming_state == ARMING_STATE_STANDBY_ERROR) {
ret = OK;
current_state->flag_fmu_armed = false;
}
break;
case ARMING_STATE_IN_AIR_RESTORE:
/* XXX implement */
break;
default:
break;
}