Merge branch 'beta' into acro2

This commit is contained in:
Anton Babushkin
2014-02-02 22:45:46 +01:00
44 changed files with 127 additions and 231 deletions
+50 -10
View File
@@ -210,7 +210,7 @@ transition_result_t set_main_state_rc(struct vehicle_status_s *status);
void set_control_mode();
void print_reject_mode(const char *msg);
void print_reject_mode(struct vehicle_status_s *current_status, const char *msg);
void print_reject_arm(const char *msg);
@@ -658,6 +658,8 @@ int commander_thread_main(int argc, char *argv[])
/* vehicle status topic */
memset(&status, 0, sizeof(status));
status.condition_landed = true; // initialize to safe value
// We want to accept RC inputs as default
status.rc_input_blocked = false;
status.main_state = MAIN_STATE_MANUAL;
status.set_nav_state = NAV_STATE_NONE;
status.set_nav_state_timestamp = 0;
@@ -927,10 +929,12 @@ int commander_thread_main(int argc, char *argv[])
check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.xy_valid, &(status.condition_local_position_valid), &status_changed);
check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.z_valid, &(status.condition_local_altitude_valid), &status_changed);
static bool published_condition_landed_fw = false;
if (status.is_rotary_wing && status.condition_local_altitude_valid) {
if (status.condition_landed != local_position.landed) {
status.condition_landed = local_position.landed;
status_changed = true;
published_condition_landed_fw = false; //make sure condition_landed is published again if the system type changes
if (status.condition_landed) {
mavlink_log_critical(mavlink_fd, "#audio: LANDED");
@@ -939,6 +943,12 @@ int commander_thread_main(int argc, char *argv[])
mavlink_log_critical(mavlink_fd, "#audio: IN AIR");
}
}
} else {
if (!published_condition_landed_fw) {
status.condition_landed = false; // Fixedwing does not have a landing detector currently
published_condition_landed_fw = true;
status_changed = true;
}
}
/* update battery status */
@@ -1097,7 +1107,7 @@ int commander_thread_main(int argc, char *argv[])
}
/* start RC input check */
if (sp_man.timestamp != 0 && hrt_absolute_time() < sp_man.timestamp + RC_TIMEOUT) {
if (!status.rc_input_blocked && sp_man.timestamp != 0 && hrt_absolute_time() < sp_man.timestamp + RC_TIMEOUT) {
/* handle the case where RC signal was regained */
if (!status.rc_signal_found_once) {
status.rc_signal_found_once = true;
@@ -1468,7 +1478,7 @@ check_mode_switches(struct manual_control_setpoint_s *sp_man, struct vehicle_sta
{
/* main mode switch */
if (!isfinite(sp_man->mode_switch)) {
warnx("mode sw not finite");
/* default to manual if signal is invalid */
status->mode_switch = MODE_SWITCH_MANUAL;
} else if (sp_man->mode_switch > STICK_ON_OFF_LIMIT) {
@@ -1550,7 +1560,7 @@ set_main_state_rc(struct vehicle_status_s *status)
break; // changed successfully or already in this state
// else fallback to SEATBELT
print_reject_mode("EASY");
print_reject_mode(status, "EASY");
}
res = main_state_transition(status, MAIN_STATE_SEATBELT);
@@ -1559,7 +1569,7 @@ set_main_state_rc(struct vehicle_status_s *status)
break; // changed successfully or already in this mode
if (status->assisted_switch != ASSISTED_SWITCH_EASY) // don't print both messages
print_reject_mode("SEATBELT");
print_reject_mode(status, "SEATBELT");
// else fallback to MANUAL
res = main_state_transition(status, MAIN_STATE_MANUAL);
@@ -1573,7 +1583,7 @@ set_main_state_rc(struct vehicle_status_s *status)
break; // changed successfully or already in this state
// else fallback to SEATBELT (EASY likely will not work too)
print_reject_mode("AUTO");
print_reject_mode(status, "AUTO");
res = main_state_transition(status, MAIN_STATE_SEATBELT);
if (res != TRANSITION_DENIED)
@@ -1592,6 +1602,7 @@ set_main_state_rc(struct vehicle_status_s *status)
}
void
set_control_mode()
{
/* set vehicle_control_mode according to main state and failsafe state */
@@ -1699,16 +1710,25 @@ set_control_mode()
}
void
print_reject_mode(const char *msg)
print_reject_mode(struct vehicle_status_s *status, const char *msg)
{
hrt_abstime t = hrt_absolute_time();
if (t - last_print_mode_reject_time > PRINT_MODE_REJECT_INTERVAL) {
last_print_mode_reject_time = t;
char s[80];
sprintf(s, "#audio: warning: reject %s", msg);
sprintf(s, "#audio: REJECT %s", msg);
mavlink_log_critical(mavlink_fd, s);
tune_negative();
// only buzz if armed, because else we're driving people nuts indoors
// they really need to look at the leds as well.
if (status->arming_state == ARMING_STATE_ARMED) {
tune_negative();
} else {
// Always show the led indication
led_negative();
}
}
}
@@ -1856,7 +1876,15 @@ void *commander_low_prio_loop(void *arg)
} else if ((int)(cmd.param4) == 1) {
/* RC calibration */
answer_command(cmd, VEHICLE_CMD_RESULT_ACCEPTED);
calib_ret = do_rc_calibration(mavlink_fd);
/* disable RC control input completely */
status.rc_input_blocked = true;
calib_ret = OK;
mavlink_log_info(mavlink_fd, "CAL: Disabling RC IN");
} else if ((int)(cmd.param4) == 2) {
/* RC trim calibration */
answer_command(cmd, VEHICLE_CMD_RESULT_ACCEPTED);
calib_ret = do_trim_calibration(mavlink_fd);
} else if ((int)(cmd.param5) == 1) {
/* accelerometer calibration */
@@ -1867,6 +1895,18 @@ void *commander_low_prio_loop(void *arg)
/* airspeed calibration */
answer_command(cmd, VEHICLE_CMD_RESULT_ACCEPTED);
calib_ret = do_airspeed_calibration(mavlink_fd);
} else if ((int)(cmd.param4) == 0) {
/* RC calibration ended - have we been in one worth confirming? */
if (status.rc_input_blocked) {
answer_command(cmd, VEHICLE_CMD_RESULT_ACCEPTED);
/* enable RC control input */
status.rc_input_blocked = false;
mavlink_log_info(mavlink_fd, "CAL: Re-enabling RC IN");
}
/* this always succeeds */
calib_ret = OK;
}
if (calib_ret == OK)
+6 -1
View File
@@ -123,11 +123,16 @@ void tune_neutral()
}
void tune_negative()
{
led_negative();
ioctl(buzzer, TONE_SET_ALARM, TONE_NOTIFY_NEGATIVE_TUNE);
}
void led_negative()
{
blink_msg_end = hrt_absolute_time() + BLINK_MSG_TIME;
rgbled_set_color(RGBLED_COLOR_RED);
rgbled_set_mode(RGBLED_MODE_BLINK_FAST);
ioctl(buzzer, TONE_SET_ALARM, TONE_NOTIFY_NEGATIVE_TUNE);
}
int tune_arm()
+3
View File
@@ -62,6 +62,9 @@ int tune_arm(void);
int tune_low_bat(void);
int tune_critical_bat(void);
void tune_stop(void);
void led_negative();
int blink_msg_state();
int led_init(void);
+5 -6
View File
@@ -53,17 +53,16 @@
#endif
static const int ERROR = -1;
int do_rc_calibration(int mavlink_fd)
int do_trim_calibration(int mavlink_fd)
{
mavlink_log_info(mavlink_fd, "trim calibration starting");
int sub_man = orb_subscribe(ORB_ID(manual_control_setpoint));
usleep(200000);
struct manual_control_setpoint_s sp;
bool changed;
orb_check(sub_man, &changed);
if (!changed) {
mavlink_log_critical(mavlink_fd, "no manual control, aborting");
mavlink_log_critical(mavlink_fd, "no inputs, aborting");
return ERROR;
}
@@ -82,12 +81,12 @@ int do_rc_calibration(int mavlink_fd)
int save_ret = param_save_default();
if (save_ret != 0) {
mavlink_log_critical(mavlink_fd, "TRIM CAL: WARN: auto-save of params failed");
mavlink_log_critical(mavlink_fd, "TRIM: SAVE FAIL");
close(sub_man);
return ERROR;
}
mavlink_log_info(mavlink_fd, "trim calibration done");
mavlink_log_info(mavlink_fd, "trim cal done");
close(sub_man);
return OK;
}
+1 -1
View File
@@ -41,6 +41,6 @@
#include <stdint.h>
int do_rc_calibration(int mavlink_fd);
int do_trim_calibration(int mavlink_fd);
#endif /* RC_CALIBRATION_H_ */
+6 -10
View File
@@ -688,7 +688,8 @@ Navigator::task_main()
/* RETURN switch, overrides MISSION switch */
if (_vstatus.return_switch == RETURN_SWITCH_RETURN) {
/* switch to RTL if not already landed after RTL and home position set */
if (!(_rtl_state == RTL_STATE_DESCEND && (myState == NAV_STATE_READY || myState == NAV_STATE_LAND)) &&
if (!(_rtl_state == RTL_STATE_DESCEND &&
(myState == NAV_STATE_READY || myState == NAV_STATE_LAND || myState == NAV_STATE_LOITER)) &&
_vstatus.condition_home_position_valid) {
dispatch(EVENT_RTL_REQUESTED);
}
@@ -746,7 +747,8 @@ Navigator::task_main()
break;
case NAV_STATE_RTL:
if (!(_rtl_state == RTL_STATE_DESCEND && (myState == NAV_STATE_READY || myState == NAV_STATE_LAND)) &&
if (!(_rtl_state == RTL_STATE_DESCEND &&
(myState == NAV_STATE_READY || myState == NAV_STATE_LAND || myState == NAV_STATE_LOITER)) &&
_vstatus.condition_home_position_valid) {
dispatch(EVENT_RTL_REQUESTED);
}
@@ -1443,14 +1445,7 @@ Navigator::check_mission_item_reached()
}
if (_mission_item.nav_cmd == NAV_CMD_LAND) {
if (_vstatus.is_rotary_wing) {
return _vstatus.condition_landed;
} else {
/* For fw there is currently no landing detector:
* make sure control is not stopped when overshooting the landing waypoint */
return false;
}
return _vstatus.condition_landed;
}
/* XXX TODO count turns */
@@ -1580,6 +1575,7 @@ Navigator::on_mission_item_reached()
dispatch(EVENT_LAND_REQUESTED);
} else {
_reset_loiter_pos = false;
dispatch(EVENT_LOITER_REQUESTED);
}
+1 -1
View File
@@ -60,4 +60,4 @@ PARAM_DEFINE_INT32(NAV_ONB_MIS_EN, 0);
PARAM_DEFINE_FLOAT(NAV_TAKEOFF_ALT, 10.0f); // default TAKEOFF altitude
PARAM_DEFINE_FLOAT(NAV_LAND_ALT, 5.0f); // slow descend from this altitude when landing
PARAM_DEFINE_FLOAT(NAV_RTL_ALT, 30.0f); // min altitude for going home in RTL mode
PARAM_DEFINE_FLOAT(NAV_RTL_LAND_T, 10.0f); // delay after descend before landing
PARAM_DEFINE_FLOAT(NAV_RTL_LAND_T, -1.0f); // delay after descend before landing, if set to -1 the system will not land but loiter at NAV_LAND_ALT
+20 -19
View File
@@ -1,7 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
* Author: Lorenz Meier <lm@inf.ethz.ch>
* Copyright (c) 2012-2014 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@@ -639,37 +638,39 @@ Sensors::parameters_update()
if (!rc_valid)
warnx("WARNING WARNING WARNING\n\nRC CALIBRATION NOT SANE!\n\n");
const char *paramerr = "FAIL PARM LOAD";
/* channel mapping */
if (param_get(_parameter_handles.rc_map_roll, &(_parameters.rc_map_roll)) != OK) {
warnx("Failed getting roll chan index");
warnx(paramerr);
}
if (param_get(_parameter_handles.rc_map_pitch, &(_parameters.rc_map_pitch)) != OK) {
warnx("Failed getting pitch chan index");
warnx(paramerr);
}
if (param_get(_parameter_handles.rc_map_yaw, &(_parameters.rc_map_yaw)) != OK) {
warnx("Failed getting yaw chan index");
warnx(paramerr);
}
if (param_get(_parameter_handles.rc_map_throttle, &(_parameters.rc_map_throttle)) != OK) {
warnx("Failed getting throttle chan index");
warnx(paramerr);
}
if (param_get(_parameter_handles.rc_map_mode_sw, &(_parameters.rc_map_mode_sw)) != OK) {
warnx("Failed getting mode sw chan index");
warnx(paramerr);
}
if (param_get(_parameter_handles.rc_map_return_sw, &(_parameters.rc_map_return_sw)) != OK) {
warnx("Failed getting return sw chan index");
warnx(paramerr);
}
if (param_get(_parameter_handles.rc_map_assisted_sw, &(_parameters.rc_map_assisted_sw)) != OK) {
warnx("Failed getting assisted sw chan index");
warnx(paramerr);
}
if (param_get(_parameter_handles.rc_map_mission_sw, &(_parameters.rc_map_mission_sw)) != OK) {
warnx("Failed getting mission sw chan index");
warnx(paramerr);
}
if (param_get(_parameter_handles.rc_map_acro_sw, &(_parameters.rc_map_acro_sw)) != OK) {
@@ -677,7 +678,7 @@ Sensors::parameters_update()
}
if (param_get(_parameter_handles.rc_map_flaps, &(_parameters.rc_map_flaps)) != OK) {
warnx("Failed getting flaps chan index");
warnx(paramerr);
}
// if (param_get(_parameter_handles.rc_map_offboard_ctrl_mode_sw, &(_parameters.rc_map_offboard_ctrl_mode_sw)) != OK) {
@@ -750,12 +751,12 @@ Sensors::parameters_update()
/* scaling of ADC ticks to battery voltage */
if (param_get(_parameter_handles.battery_voltage_scaling, &(_parameters.battery_voltage_scaling)) != OK) {
warnx("Failed updating voltage scaling param");
warnx(paramerr);
}
/* scaling of ADC ticks to battery current */
if (param_get(_parameter_handles.battery_current_scaling, &(_parameters.battery_current_scaling)) != OK) {
warnx("Failed updating current scaling param");
warnx(paramerr);
}
param_get(_parameter_handles.board_rotation, &(_parameters.board_rotation));
@@ -1664,17 +1665,17 @@ int sensors_main(int argc, char *argv[])
if (!strcmp(argv[1], "start")) {
if (sensors::g_sensors != nullptr)
errx(0, "sensors task already running");
errx(0, "already running");
sensors::g_sensors = new Sensors;
if (sensors::g_sensors == nullptr)
errx(1, "sensors task alloc failed");
errx(1, "alloc failed");
if (OK != sensors::g_sensors->start()) {
delete sensors::g_sensors;
sensors::g_sensors = nullptr;
err(1, "sensors task start failed");
err(1, "start failed");
}
exit(0);
@@ -1682,7 +1683,7 @@ int sensors_main(int argc, char *argv[])
if (!strcmp(argv[1], "stop")) {
if (sensors::g_sensors == nullptr)
errx(1, "sensors task not running");
errx(1, "not running");
delete sensors::g_sensors;
sensors::g_sensors = nullptr;
@@ -1691,10 +1692,10 @@ int sensors_main(int argc, char *argv[])
if (!strcmp(argv[1], "status")) {
if (sensors::g_sensors) {
errx(0, "task is running");
errx(0, "is running");
} else {
errx(1, "task is not running");
errx(1, "not running");
}
}
+1
View File
@@ -216,6 +216,7 @@ struct vehicle_status_s
bool rc_signal_found_once;
bool rc_signal_lost; /**< true if RC reception lost */
bool rc_input_blocked; /**< set if RC input should be ignored */
bool offboard_control_signal_found_once;
bool offboard_control_signal_lost;