diff options
Diffstat (limited to 'src/modules/commander')
-rw-r--r-- | src/modules/commander/accelerometer_calibration.cpp | 3 | ||||
-rw-r--r-- | src/modules/commander/accelerometer_calibration.h | 3 | ||||
-rw-r--r-- | src/modules/commander/airspeed_calibration.cpp | 132 | ||||
-rw-r--r-- | src/modules/commander/airspeed_calibration.h | 2 | ||||
-rw-r--r-- | src/modules/commander/baro_calibration.cpp | 2 | ||||
-rw-r--r-- | src/modules/commander/baro_calibration.h | 2 | ||||
-rw-r--r-- | src/modules/commander/calibration_messages.h | 3 | ||||
-rw-r--r-- | src/modules/commander/calibration_routines.cpp | 3 | ||||
-rw-r--r-- | src/modules/commander/calibration_routines.h | 3 | ||||
-rw-r--r-- | src/modules/commander/commander.cpp | 237 | ||||
-rw-r--r-- | src/modules/commander/commander_helper.cpp | 10 | ||||
-rw-r--r-- | src/modules/commander/commander_helper.h | 9 | ||||
-rw-r--r-- | src/modules/commander/mag_calibration.h | 2 | ||||
-rw-r--r-- | src/modules/commander/state_machine_helper.cpp | 75 | ||||
-rw-r--r-- | src/modules/commander/state_machine_helper.h | 12 |
15 files changed, 314 insertions, 184 deletions
diff --git a/src/modules/commander/accelerometer_calibration.cpp b/src/modules/commander/accelerometer_calibration.cpp index be465ab76..7a4e7a766 100644 --- a/src/modules/commander/accelerometer_calibration.cpp +++ b/src/modules/commander/accelerometer_calibration.cpp @@ -1,7 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. - * Author: Anton Babushkin <anton.babushkin@me.com> + * Copyright (c) 2013 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 diff --git a/src/modules/commander/accelerometer_calibration.h b/src/modules/commander/accelerometer_calibration.h index 1cf9c0977..6b7e16d44 100644 --- a/src/modules/commander/accelerometer_calibration.h +++ b/src/modules/commander/accelerometer_calibration.h @@ -1,7 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. - * Author: Anton Babushkin <anton.babushkin@me.com> + * Copyright (c) 2013 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 diff --git a/src/modules/commander/airspeed_calibration.cpp b/src/modules/commander/airspeed_calibration.cpp index 5d21d89d0..598cfe9e2 100644 --- a/src/modules/commander/airspeed_calibration.cpp +++ b/src/modules/commander/airspeed_calibration.cpp @@ -51,6 +51,7 @@ #include <mavlink/mavlink_log.h> #include <systemlib/param/param.h> #include <systemlib/err.h> +#include <systemlib/airspeed.h> /* oddly, ERROR is not defined for c++ */ #ifdef ERROR @@ -64,19 +65,17 @@ int do_airspeed_calibration(int mavlink_fd) { /* give directions */ mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name); - mavlink_log_info(mavlink_fd, "ensure airspeed sensor is not registering wind"); - const int calibration_count = 2000; + const unsigned calibration_count = 2000; int diff_pres_sub = orb_subscribe(ORB_ID(differential_pressure)); struct differential_pressure_s diff_pres; - int calibration_counter = 0; float diff_pres_offset = 0.0f; /* Reset sensor parameters */ struct airspeed_scale airscale = { - 0.0f, + diff_pres_offset, 1.0f, }; @@ -95,12 +94,29 @@ int do_airspeed_calibration(int mavlink_fd) } if (!paramreset_successful) { - warn("FAILED to set scale / offsets for airspeed"); - mavlink_log_critical(mavlink_fd, "dpress reset failed"); - mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name); - return ERROR; + + /* only warn if analog scaling is zero */ + float analog_scaling = 0.0f; + param_get(param_find("SENS_DPRES_ANSC"), &(analog_scaling)); + if (fabsf(analog_scaling) < 0.1f) { + mavlink_log_critical(mavlink_fd, "If analog sens, retry with [SENS_DPRES_ANSC=1000]"); + close(diff_pres_sub); + return ERROR; + } + + /* set scaling offset parameter */ + if (param_set(param_find("SENS_DPRES_OFF"), &(diff_pres_offset))) { + mavlink_log_critical(mavlink_fd, CAL_FAILED_SET_PARAMS_MSG); + close(diff_pres_sub); + return ERROR; + } } + unsigned calibration_counter = 0; + + mavlink_log_critical(mavlink_fd, "Ensure sensor is not measuring wind"); + usleep(500 * 1000); + while (calibration_counter < calibration_count) { /* wait blocking for new data */ @@ -112,11 +128,12 @@ int do_airspeed_calibration(int mavlink_fd) if (poll_ret) { orb_copy(ORB_ID(differential_pressure), diff_pres_sub, &diff_pres); + diff_pres_offset += diff_pres.differential_pressure_raw_pa; calibration_counter++; if (calibration_counter % (calibration_count / 20) == 0) { - mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, (calibration_counter * 100) / calibration_count); + mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, (calibration_counter * 80) / calibration_count); } } else if (poll_ret == 0) { @@ -131,6 +148,16 @@ int do_airspeed_calibration(int mavlink_fd) if (isfinite(diff_pres_offset)) { + int fd_scale = open(AIRSPEED_DEVICE_PATH, 0); + airscale.offset_pa = diff_pres_offset; + if (fd_scale > 0) { + if (OK != ioctl(fd_scale, AIRSPEEDIOCSSCALE, (long unsigned int)&airscale)) { + mavlink_log_critical(mavlink_fd, "airspeed offset update failed"); + } + + close(fd_scale); + } + if (param_set(param_find("SENS_DPRES_OFF"), &(diff_pres_offset))) { mavlink_log_critical(mavlink_fd, CAL_FAILED_SET_PARAMS_MSG); close(diff_pres_sub); @@ -147,14 +174,91 @@ int do_airspeed_calibration(int mavlink_fd) return ERROR; } - mavlink_log_info(mavlink_fd, CAL_DONE_MSG, sensor_name); - tune_neutral(true); - close(diff_pres_sub); - return OK; - } else { mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name); close(diff_pres_sub); return ERROR; } + + mavlink_log_critical(mavlink_fd, "Offset of %d Pa, create airflow now!", (int)diff_pres_offset); + + /* wait 500 ms to ensure parameter propagated through the system */ + usleep(500 * 1000); + + calibration_counter = 0; + const int maxcount = 3000; + + /* just take a few samples and make sure pitot tubes are not reversed, timeout after ~30 seconds */ + while (calibration_counter < maxcount) { + + /* wait blocking for new data */ + struct pollfd fds[1]; + fds[0].fd = diff_pres_sub; + fds[0].events = POLLIN; + + int poll_ret = poll(fds, 1, 1000); + + if (poll_ret) { + orb_copy(ORB_ID(differential_pressure), diff_pres_sub, &diff_pres); + + calibration_counter++; + + if (fabsf(diff_pres.differential_pressure_raw_pa) < 50.0f) { + if (calibration_counter % 100 == 0) { + mavlink_log_critical(mavlink_fd, "Missing airflow! (%d, wanted: 50 Pa, #h101)", + (int)diff_pres.differential_pressure_raw_pa); + } + continue; + } + + /* do not allow negative values */ + if (diff_pres.differential_pressure_raw_pa < 0.0f) { + mavlink_log_info(mavlink_fd, "negative pressure: ERROR (%d Pa)", + (int)diff_pres.differential_pressure_raw_pa); + mavlink_log_critical(mavlink_fd, "%d Pa: swap static and dynamic ports!", (int)diff_pres.differential_pressure_raw_pa); + close(diff_pres_sub); + + /* the user setup is wrong, wipe the calibration to force a proper re-calibration */ + + diff_pres_offset = 0.0f; + if (param_set(param_find("SENS_DPRES_OFF"), &(diff_pres_offset))) { + mavlink_log_critical(mavlink_fd, CAL_FAILED_SET_PARAMS_MSG); + close(diff_pres_sub); + return ERROR; + } + + /* save */ + mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 0); + (void)param_save_default(); + + close(diff_pres_sub); + + mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name); + return ERROR; + } else { + mavlink_log_info(mavlink_fd, "positive pressure: OK (%d Pa)", + (int)diff_pres.differential_pressure_raw_pa); + break; + } + + } else if (poll_ret == 0) { + /* any poll failure for 1s is a reason to abort */ + mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name); + close(diff_pres_sub); + return ERROR; + } + } + + if (calibration_counter == maxcount) { + mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name); + close(diff_pres_sub); + return ERROR; + } + + mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 100); + + mavlink_log_info(mavlink_fd, CAL_DONE_MSG, sensor_name); + tune_neutral(true); + close(diff_pres_sub); + return OK; } diff --git a/src/modules/commander/airspeed_calibration.h b/src/modules/commander/airspeed_calibration.h index 71c701fc2..8c6b65ff1 100644 --- a/src/modules/commander/airspeed_calibration.h +++ b/src/modules/commander/airspeed_calibration.h @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * Copyright (c) 2013, 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 diff --git a/src/modules/commander/baro_calibration.cpp b/src/modules/commander/baro_calibration.cpp index 3123c4087..da98644b4 100644 --- a/src/modules/commander/baro_calibration.cpp +++ b/src/modules/commander/baro_calibration.cpp @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * Copyright (c) 2013 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 diff --git a/src/modules/commander/baro_calibration.h b/src/modules/commander/baro_calibration.h index bc42bc6cf..ce78ae700 100644 --- a/src/modules/commander/baro_calibration.h +++ b/src/modules/commander/baro_calibration.h @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * Copyright (c) 2013 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 diff --git a/src/modules/commander/calibration_messages.h b/src/modules/commander/calibration_messages.h index fd8b8564d..b1e209efc 100644 --- a/src/modules/commander/calibration_messages.h +++ b/src/modules/commander/calibration_messages.h @@ -1,7 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. - * Author: Anton Babushkin <anton.babushkin@me.com> + * Copyright (c) 2013 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 diff --git a/src/modules/commander/calibration_routines.cpp b/src/modules/commander/calibration_routines.cpp index 43f341ae7..5796204bf 100644 --- a/src/modules/commander/calibration_routines.cpp +++ b/src/modules/commander/calibration_routines.cpp @@ -1,7 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: Lorenz Meier <lm@inf.ethz.ch> + * Copyright (c) 2012 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 diff --git a/src/modules/commander/calibration_routines.h b/src/modules/commander/calibration_routines.h index e3e7fbafd..3c8e49ee9 100644 --- a/src/modules/commander/calibration_routines.h +++ b/src/modules/commander/calibration_routines.h @@ -1,7 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: Lorenz Meier <lm@inf.ethz.ch> + * Copyright (c) 2012 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 diff --git a/src/modules/commander/commander.cpp b/src/modules/commander/commander.cpp index e925b8ed7..c11286789 100644 --- a/src/modules/commander/commander.cpp +++ b/src/modules/commander/commander.cpp @@ -78,6 +78,7 @@ #include <uORB/topics/differential_pressure.h> #include <uORB/topics/safety.h> #include <uORB/topics/system_power.h> +#include <uORB/topics/mission.h> #include <uORB/topics/mission_result.h> #include <uORB/topics/telemetry_status.h> @@ -92,6 +93,7 @@ #include <systemlib/cpuload.h> #include <systemlib/rc_check.h> #include <systemlib/state_table.h> +#include <dataman/dataman.h> #include "px4_custom_mode.h" #include "commander_helper.h" @@ -286,15 +288,22 @@ int commander_main(int argc, char *argv[]) exit(0); } - if (!strcmp(argv[1], "status")) { - if (thread_running) { - warnx("\tcommander is running"); - print_status(); + /* commands needing the app to run below */ + if (!thread_running) { + warnx("\tcommander not started"); + exit(1); + } - } else { - warnx("\tcommander not started"); - } + if (!strcmp(argv[1], "status")) { + print_status(); + exit(0); + } + if (!strcmp(argv[1], "check")) { + int mavlink_fd_local = open(MAVLINK_LOG_DEVICE, 0); + int checkres = prearm_check(&status, mavlink_fd_local); + close(mavlink_fd_local); + warnx("FINAL RESULT: %s", (checkres == 0) ? "OK" : "FAILED"); exit(0); } @@ -303,7 +312,7 @@ int commander_main(int argc, char *argv[]) exit(0); } - if (!strcmp(argv[1], "2")) { + if (!strcmp(argv[1], "disarm")) { arm_disarm(false, mavlink_fd, "command line"); exit(0); } @@ -324,6 +333,7 @@ void usage(const char *reason) void print_status() { + warnx("type: %s", (status.is_rotary_wing) ? "ROTARY" : "PLANE"); warnx("usb powered: %s", (on_usb_power) ? "yes" : "no"); /* read all relevant states */ @@ -393,10 +403,12 @@ transition_result_t arm_disarm(bool arm, const int mavlink_fd_local, const char return arming_res; } -bool handle_command(struct vehicle_status_s *status, const struct safety_s *safety, struct vehicle_command_s *cmd, struct actuator_armed_s *armed, struct home_position_s *home, struct vehicle_global_position_s *global_pos, orb_advert_t *home_pub) +bool handle_command(struct vehicle_status_s *status_local, const struct safety_s *safety_local, + struct vehicle_command_s *cmd, struct actuator_armed_s *armed_local, + struct home_position_s *home, struct vehicle_global_position_s *global_pos, orb_advert_t *home_pub) { /* only handle commands that are meant to be handled by this system and component */ - if (cmd->target_system != status->system_id || ((cmd->target_component != status->component_id) && (cmd->target_component != 0))) { // component_id 0: valid for all components + if (cmd->target_system != status_local->system_id || ((cmd->target_component != status_local->component_id) && (cmd->target_component != 0))) { // component_id 0: valid for all components return false; } @@ -415,7 +427,7 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe /* set HIL state */ hil_state_t new_hil_state = (base_mode & MAV_MODE_FLAG_HIL_ENABLED) ? HIL_STATE_ON : HIL_STATE_OFF; - transition_result_t hil_ret = hil_state_transition(new_hil_state, status_pub, status, mavlink_fd); + transition_result_t hil_ret = hil_state_transition(new_hil_state, status_pub, status_local, mavlink_fd); // Transition the arming state arming_ret = arm_disarm(base_mode & MAV_MODE_FLAG_SAFETY_ARMED, mavlink_fd, "set mode command"); @@ -424,43 +436,43 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe /* use autopilot-specific mode */ if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_MANUAL) { /* MANUAL */ - main_ret = main_state_transition(status, MAIN_STATE_MANUAL); + main_ret = main_state_transition(status_local, MAIN_STATE_MANUAL); } else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_ALTCTL) { /* ALTCTL */ - main_ret = main_state_transition(status, MAIN_STATE_ALTCTL); + main_ret = main_state_transition(status_local, MAIN_STATE_ALTCTL); } else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_POSCTL) { /* POSCTL */ - main_ret = main_state_transition(status, MAIN_STATE_POSCTL); + main_ret = main_state_transition(status_local, MAIN_STATE_POSCTL); } else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_AUTO) { /* AUTO */ - main_ret = main_state_transition(status, MAIN_STATE_AUTO_MISSION); + main_ret = main_state_transition(status_local, MAIN_STATE_AUTO_MISSION); } else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_ACRO) { /* ACRO */ - main_ret = main_state_transition(status, MAIN_STATE_ACRO); + main_ret = main_state_transition(status_local, MAIN_STATE_ACRO); } else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_OFFBOARD) { /* OFFBOARD */ - main_ret = main_state_transition(status, MAIN_STATE_OFFBOARD); + main_ret = main_state_transition(status_local, MAIN_STATE_OFFBOARD); } } else { /* use base mode */ if (base_mode & MAV_MODE_FLAG_AUTO_ENABLED) { /* AUTO */ - main_ret = main_state_transition(status, MAIN_STATE_AUTO_MISSION); + main_ret = main_state_transition(status_local, MAIN_STATE_AUTO_MISSION); } else if (base_mode & MAV_MODE_FLAG_MANUAL_INPUT_ENABLED) { if (base_mode & MAV_MODE_FLAG_GUIDED_ENABLED) { /* POSCTL */ - main_ret = main_state_transition(status, MAIN_STATE_POSCTL); + main_ret = main_state_transition(status_local, MAIN_STATE_POSCTL); } else if (base_mode & MAV_MODE_FLAG_STABILIZE_ENABLED) { /* MANUAL */ - main_ret = main_state_transition(status, MAIN_STATE_MANUAL); + main_ret = main_state_transition(status_local, MAIN_STATE_MANUAL); } } } @@ -475,22 +487,25 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe break; case VEHICLE_CMD_COMPONENT_ARM_DISARM: { - // Follow exactly what the mavlink spec says for values: 0.0f for disarm, 1.0f for arm. - // We use an float epsilon delta to test float equality. - if (cmd->param1 != 0.0f && (fabsf(cmd->param1 - 1.0f) > 2.0f * FLT_EPSILON)) { - mavlink_log_info(mavlink_fd, "Unsupported ARM_DISARM parameter: %.6f", (double)cmd->param1); + // Adhere to MAVLink specs, but base on knowledge that these fundamentally encode ints + // for logic state parameters + + if (static_cast<int>(cmd->param1 + 0.5f) != 0 && static_cast<int>(cmd->param1 + 0.5f) != 1) { + mavlink_log_critical(mavlink_fd, "Unsupported ARM_DISARM param: %.3f", (double)cmd->param1); } else { + bool cmd_arms = (static_cast<int>(cmd->param1 + 0.5f) == 1); + // Flick to inair restore first if this comes from an onboard system - if (cmd->source_system == status->system_id && cmd->source_component == status->component_id) { - status->arming_state = ARMING_STATE_IN_AIR_RESTORE; + if (cmd->source_system == status_local->system_id && cmd->source_component == status_local->component_id) { + status_local->arming_state = ARMING_STATE_IN_AIR_RESTORE; } - transition_result_t arming_res = arm_disarm(cmd->param1 != 0.0f, mavlink_fd, "arm/disarm component command"); + transition_result_t arming_res = arm_disarm(cmd_arms, mavlink_fd, "arm/disarm component command"); if (arming_res == TRANSITION_DENIED) { - mavlink_log_critical(mavlink_fd, "#audio: REJECTING component arm cmd"); + mavlink_log_critical(mavlink_fd, "REJECTING component arm cmd"); cmd_result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; } else { @@ -502,20 +517,24 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe case VEHICLE_CMD_OVERRIDE_GOTO: { // TODO listen vehicle_command topic directly from navigator (?) - unsigned int mav_goto = cmd->param1; + + // Increase by 0.5f and rely on the integer cast + // implicit floor(). This is the *safest* way to + // convert from floats representing small ints to actual ints. + unsigned int mav_goto = (cmd->param1 + 0.5f); if (mav_goto == 0) { // MAV_GOTO_DO_HOLD - status->nav_state = NAVIGATION_STATE_AUTO_LOITER; - mavlink_log_critical(mavlink_fd, "#audio: pause mission cmd"); + status_local->nav_state = NAVIGATION_STATE_AUTO_LOITER; + mavlink_log_critical(mavlink_fd, "Pause mission cmd"); cmd_result = VEHICLE_CMD_RESULT_ACCEPTED; } else if (mav_goto == 1) { // MAV_GOTO_DO_CONTINUE - status->nav_state = NAVIGATION_STATE_AUTO_MISSION; - mavlink_log_critical(mavlink_fd, "#audio: continue mission cmd"); + status_local->nav_state = NAVIGATION_STATE_AUTO_MISSION; + mavlink_log_critical(mavlink_fd, "Continue mission cmd"); cmd_result = VEHICLE_CMD_RESULT_ACCEPTED; } else { - mavlink_log_info(mavlink_fd, "Unsupported OVERRIDE_GOTO: %f %f %f %f %f %f %f %f", + mavlink_log_critical(mavlink_fd, "REJ CMD: %.1f %.1f %.1f %.1f %.1f %.1f %.1f %.1f", (double)cmd->param1, (double)cmd->param2, (double)cmd->param3, @@ -533,7 +552,7 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe //XXX: to enable the parachute, a param needs to be set //xxx: for safety only for now, param3 is unused by VEHICLE_CMD_DO_SET_SERVO - if (armed->armed && cmd->param3 > 0.5 && parachute_enabled) { + if (armed_local->armed && cmd->param3 > 0.5 && parachute_enabled) { transition_result_t failsafe_res = failsafe_state_transition(status, FAILSAFE_STATE_TERMINATION); cmd_result = VEHICLE_CMD_RESULT_ACCEPTED; @@ -551,7 +570,7 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe if (use_current) { /* use current position */ - if (status->condition_global_position_valid) { + if (status_local->condition_global_position_valid) { home->lat = global_pos->lat; home->lon = global_pos->lon; home->alt = global_pos->alt; @@ -588,7 +607,7 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe } /* mark home position as set */ - status->condition_home_position_valid = true; + status_local->condition_home_position_valid = true; } } break; @@ -678,11 +697,11 @@ int commander_thread_main(int argc, char *argv[]) /* initialize */ if (led_init() != 0) { - warnx("ERROR: Failed to initialize leds"); + warnx("ERROR: LED INIT FAIL"); } if (buzzer_init() != OK) { - warnx("ERROR: Failed to initialize buzzer"); + warnx("ERROR: BUZZER INIT FAIL"); } mavlink_fd = open(MAVLINK_LOG_DEVICE, 0); @@ -725,6 +744,11 @@ int commander_thread_main(int argc, char *argv[]) /* publish initial state */ status_pub = orb_advertise(ORB_ID(vehicle_status), &status); + if (status_pub < 0) { + warnx("ERROR: orb_advertise for topic vehicle_status failed (uorb app running?).\n"); + warnx("exiting."); + exit(ERROR); + } /* armed topic */ orb_advert_t armed_pub; @@ -742,13 +766,29 @@ int commander_thread_main(int argc, char *argv[]) struct home_position_s home; memset(&home, 0, sizeof(home)); - if (status_pub < 0) { - warnx("ERROR: orb_advertise for topic vehicle_status failed (uorb app running?).\n"); - warnx("exiting."); - exit(ERROR); - } + /* init mission state, do it here to allow navigator to use stored mission even if mavlink failed to start */ + orb_advert_t mission_pub = -1; + mission_s mission; + if (dm_read(DM_KEY_MISSION_STATE, 0, &mission, sizeof(mission_s)) == sizeof(mission_s)) { + if (mission.dataman_id >= 0 && mission.dataman_id <= 1) { + warnx("loaded mission state: dataman_id=%d, count=%u, current=%d", mission.dataman_id, mission.count, mission.current_seq); + mavlink_log_info(mavlink_fd, "[cmd] dataman_id=%d, count=%u, current=%d", + mission.dataman_id, mission.count, mission.current_seq); + } else { + const char *missionfail = "reading mission state failed"; + warnx("%s", missionfail); + mavlink_log_critical(mavlink_fd, missionfail); - mavlink_log_info(mavlink_fd, "[cmd] started"); + /* initialize mission state in dataman */ + mission.dataman_id = 0; + mission.count = 0; + mission.current_seq = 0; + dm_write(DM_KEY_MISSION_STATE, 0, DM_PERSIST_POWER_ON_RESET, &mission, sizeof(mission_s)); + } + + mission_pub = orb_advertise(ORB_ID(offboard_mission), &mission); + orb_publish(ORB_ID(offboard_mission), mission_pub, &mission); + } int ret; @@ -1042,7 +1082,7 @@ int commander_thread_main(int argc, char *argv[]) arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY : ARMING_STATE_STANDBY_ERROR); if (TRANSITION_CHANGED == arming_state_transition(&status, &safety, new_arming_state, &armed, mavlink_fd)) { - mavlink_log_info(mavlink_fd, "[cmd] DISARMED by safety switch"); + mavlink_log_info(mavlink_fd, "DISARMED by safety switch"); arming_state_changed = true; } } @@ -1146,10 +1186,10 @@ int commander_thread_main(int argc, char *argv[]) status_changed = true; if (status.condition_landed) { - mavlink_log_critical(mavlink_fd, "#audio: LANDED"); + mavlink_log_critical(mavlink_fd, "LANDED MODE"); } else { - mavlink_log_critical(mavlink_fd, "#audio: IN AIR"); + mavlink_log_critical(mavlink_fd, "IN AIR MODE"); } } } @@ -1229,14 +1269,14 @@ int commander_thread_main(int argc, char *argv[]) /* if battery voltage is getting lower, warn using buzzer, etc. */ if (status.condition_battery_voltage_valid && status.battery_remaining < 0.25f && !low_battery_voltage_actions_done) { low_battery_voltage_actions_done = true; - mavlink_log_critical(mavlink_fd, "#audio: WARNING: LOW BATTERY"); + mavlink_log_critical(mavlink_fd, "LOW BATTERY, RETURN TO LAND ADVISED"); status.battery_warning = VEHICLE_BATTERY_WARNING_LOW; status_changed = true; } else if (status.condition_battery_voltage_valid && status.battery_remaining < 0.1f && !critical_battery_voltage_actions_done && low_battery_voltage_actions_done) { /* critical battery voltage, this is rather an emergency, change state machine */ critical_battery_voltage_actions_done = true; - mavlink_log_critical(mavlink_fd, "#audio: EMERGENCY: CRITICAL BATTERY"); + mavlink_log_emergency(mavlink_fd, "CRITICAL BATTERY, LAND IMMEDIATELY"); status.battery_warning = VEHICLE_BATTERY_WARNING_CRITICAL; if (armed.armed) { @@ -1298,12 +1338,12 @@ int commander_thread_main(int argc, char *argv[]) /* handle the case where RC signal was regained */ if (!status.rc_signal_found_once) { status.rc_signal_found_once = true; - mavlink_log_critical(mavlink_fd, "#audio: detected RC signal first time"); + mavlink_log_critical(mavlink_fd, "detected RC signal first time"); status_changed = true; } else { if (status.rc_signal_lost) { - mavlink_log_critical(mavlink_fd, "#audio: RC signal regained"); + mavlink_log_critical(mavlink_fd, "RC signal regained"); status_changed = true; } } @@ -1344,7 +1384,7 @@ int commander_thread_main(int argc, char *argv[]) * the system can be armed in auto if armed via the GCS. */ if (status.main_state != MAIN_STATE_MANUAL) { - print_reject_arm("#audio: NOT ARMING: Switch to MANUAL mode first."); + print_reject_arm("NOT ARMING: Switch to MANUAL mode first."); } else { arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed, mavlink_fd); if (arming_ret == TRANSITION_CHANGED) { @@ -1364,16 +1404,16 @@ int commander_thread_main(int argc, char *argv[]) if (arming_ret == TRANSITION_CHANGED) { if (status.arming_state == ARMING_STATE_ARMED) { - mavlink_log_info(mavlink_fd, "[cmd] ARMED by RC"); + mavlink_log_info(mavlink_fd, "ARMED by RC"); } else { - mavlink_log_info(mavlink_fd, "[cmd] DISARMED by RC"); + mavlink_log_info(mavlink_fd, "DISARMED by RC"); } arming_state_changed = true; } else if (arming_ret == TRANSITION_DENIED) { /* DENIED here indicates bug in the commander */ - mavlink_log_critical(mavlink_fd, "ERROR: arming state transition denied"); + mavlink_log_critical(mavlink_fd, "arming state transition denied"); tune_negative(true); } @@ -1387,12 +1427,12 @@ int commander_thread_main(int argc, char *argv[]) } else if (main_res == TRANSITION_DENIED) { /* DENIED here indicates bug in the commander */ - mavlink_log_critical(mavlink_fd, "ERROR: main state transition denied"); + mavlink_log_critical(mavlink_fd, "main state transition denied"); } } else { if (!status.rc_signal_lost) { - mavlink_log_critical(mavlink_fd, "#audio: CRITICAL: RC SIGNAL LOST"); + mavlink_log_critical(mavlink_fd, "RC SIGNAL LOST"); status.rc_signal_lost = true; status_changed = true; } @@ -1404,14 +1444,14 @@ int commander_thread_main(int argc, char *argv[]) if (hrt_elapsed_time(&telemetry_last_heartbeat[i]) < DL_TIMEOUT) { /* handle the case where data link was regained */ if (telemetry_lost[i]) { - mavlink_log_critical(mavlink_fd, "#audio: data link %i regained", i); + mavlink_log_critical(mavlink_fd, "data link %i regained", i); telemetry_lost[i] = false; } have_link = true; } else { if (!telemetry_lost[i]) { - mavlink_log_critical(mavlink_fd, "#audio: data link %i lost", i); + mavlink_log_critical(mavlink_fd, "data link %i lost", i); telemetry_lost[i] = true; } } @@ -1426,7 +1466,7 @@ int commander_thread_main(int argc, char *argv[]) } else { if (!status.data_link_lost) { - mavlink_log_critical(mavlink_fd, "#audio: CRITICAL: ALL DATA LINKS LOST"); + mavlink_log_critical(mavlink_fd, "ALL DATA LINKS LOST"); status.data_link_lost = true; status_changed = true; } @@ -1486,7 +1526,7 @@ int commander_thread_main(int argc, char *argv[]) /* now set navigation state according to failsafe and main state */ bool nav_state_changed = set_nav_state(&status, (bool)datalink_loss_enabled, - mission_result.mission_finished); + mission_result.finished); // TODO handle mode changes by commands if (main_state_changed) { @@ -1590,6 +1630,7 @@ int commander_thread_main(int argc, char *argv[]) close(diff_pres_sub); close(param_changed_sub); close(battery_sub); + close(mission_pub); thread_running = false; @@ -1609,22 +1650,22 @@ check_valid(hrt_abstime timestamp, hrt_abstime timeout, bool valid_in, bool *val } void -control_status_leds(vehicle_status_s *status, const actuator_armed_s *actuator_armed, bool changed) +control_status_leds(vehicle_status_s *status_local, const actuator_armed_s *actuator_armed, bool changed) { /* driving rgbled */ if (changed) { bool set_normal_color = false; /* set mode */ - if (status->arming_state == ARMING_STATE_ARMED) { + if (status_local->arming_state == ARMING_STATE_ARMED) { rgbled_set_mode(RGBLED_MODE_ON); set_normal_color = true; - } else if (status->arming_state == ARMING_STATE_ARMED_ERROR) { + } else if (status_local->arming_state == ARMING_STATE_ARMED_ERROR) { rgbled_set_mode(RGBLED_MODE_BLINK_FAST); rgbled_set_color(RGBLED_COLOR_RED); - } else if (status->arming_state == ARMING_STATE_STANDBY) { + } else if (status_local->arming_state == ARMING_STATE_STANDBY) { rgbled_set_mode(RGBLED_MODE_BREATHE); set_normal_color = true; @@ -1635,12 +1676,12 @@ control_status_leds(vehicle_status_s *status, const actuator_armed_s *actuator_a if (set_normal_color) { /* set color */ - if (status->battery_warning == VEHICLE_BATTERY_WARNING_LOW || status->failsafe) { + if (status_local->battery_warning == VEHICLE_BATTERY_WARNING_LOW || status_local->failsafe) { rgbled_set_color(RGBLED_COLOR_AMBER); /* VEHICLE_BATTERY_WARNING_CRITICAL handled as ARMING_STATE_ARMED_ERROR / ARMING_STATE_STANDBY_ERROR */ } else { - if (status->condition_local_position_valid) { + if (status_local->condition_local_position_valid) { rgbled_set_color(RGBLED_COLOR_GREEN); } else { @@ -1673,7 +1714,7 @@ control_status_leds(vehicle_status_s *status, const actuator_armed_s *actuator_a #endif /* give system warnings on error LED, XXX maybe add memory usage warning too */ - if (status->load > 0.95f) { + if (status_local->load > 0.95f) { if (leds_counter % 2 == 0) { led_toggle(LED_AMBER); } @@ -1686,16 +1727,16 @@ control_status_leds(vehicle_status_s *status, const actuator_armed_s *actuator_a } transition_result_t -set_main_state_rc(struct vehicle_status_s *status, struct manual_control_setpoint_s *sp_man) +set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_setpoint_s *sp_man) { /* set main state according to RC switches */ transition_result_t res = TRANSITION_DENIED; /* offboard switch overrides main switch */ if (sp_man->offboard_switch == SWITCH_POS_ON) { - res = main_state_transition(status, MAIN_STATE_OFFBOARD); + res = main_state_transition(status_local, MAIN_STATE_OFFBOARD); if (res == TRANSITION_DENIED) { - print_reject_mode(status, "OFFBOARD"); + print_reject_mode(status_local, "OFFBOARD"); } else { return res; @@ -1710,78 +1751,78 @@ set_main_state_rc(struct vehicle_status_s *status, struct manual_control_setpoin case SWITCH_POS_OFF: // MANUAL if (sp_man->acro_switch == SWITCH_POS_ON) { - res = main_state_transition(status, MAIN_STATE_ACRO); + res = main_state_transition(status_local, MAIN_STATE_ACRO); } else { - res = main_state_transition(status, MAIN_STATE_MANUAL); + res = main_state_transition(status_local, MAIN_STATE_MANUAL); } // TRANSITION_DENIED is not possible here break; case SWITCH_POS_MIDDLE: // ASSIST if (sp_man->posctl_switch == SWITCH_POS_ON) { - res = main_state_transition(status, MAIN_STATE_POSCTL); + res = main_state_transition(status_local, MAIN_STATE_POSCTL); if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state } - print_reject_mode(status, "POSCTL"); + print_reject_mode(status_local, "POSCTL"); } // fallback to ALTCTL - res = main_state_transition(status, MAIN_STATE_ALTCTL); + res = main_state_transition(status_local, MAIN_STATE_ALTCTL); if (res != TRANSITION_DENIED) { break; // changed successfully or already in this mode } if (sp_man->posctl_switch != SWITCH_POS_ON) { - print_reject_mode(status, "ALTCTL"); + print_reject_mode(status_local, "ALTCTL"); } // fallback to MANUAL - res = main_state_transition(status, MAIN_STATE_MANUAL); + res = main_state_transition(status_local, MAIN_STATE_MANUAL); // TRANSITION_DENIED is not possible here break; case SWITCH_POS_ON: // AUTO if (sp_man->return_switch == SWITCH_POS_ON) { - res = main_state_transition(status, MAIN_STATE_AUTO_RTL); + res = main_state_transition(status_local, MAIN_STATE_AUTO_RTL); if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state } - print_reject_mode(status, "AUTO_RTL"); + print_reject_mode(status_local, "AUTO_RTL"); // fallback to LOITER if home position not set - res = main_state_transition(status, MAIN_STATE_AUTO_LOITER); + res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER); if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state } } else if (sp_man->loiter_switch == SWITCH_POS_ON) { - res = main_state_transition(status, MAIN_STATE_AUTO_LOITER); + res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER); if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state } - print_reject_mode(status, "AUTO_LOITER"); + print_reject_mode(status_local, "AUTO_LOITER"); } else { - res = main_state_transition(status, MAIN_STATE_AUTO_MISSION); + res = main_state_transition(status_local, MAIN_STATE_AUTO_MISSION); if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state } - print_reject_mode(status, "AUTO_MISSION"); + print_reject_mode(status_local, "AUTO_MISSION"); // fallback to LOITER if home position not set - res = main_state_transition(status, MAIN_STATE_AUTO_LOITER); + res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER); if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state @@ -1789,21 +1830,21 @@ set_main_state_rc(struct vehicle_status_s *status, struct manual_control_setpoin } // fallback to POSCTL - res = main_state_transition(status, MAIN_STATE_POSCTL); + res = main_state_transition(status_local, MAIN_STATE_POSCTL); if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state } // fallback to ALTCTL - res = main_state_transition(status, MAIN_STATE_ALTCTL); + res = main_state_transition(status_local, MAIN_STATE_ALTCTL); if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state } // fallback to MANUAL - res = main_state_transition(status, MAIN_STATE_MANUAL); + res = main_state_transition(status_local, MAIN_STATE_MANUAL); // TRANSITION_DENIED is not possible here break; @@ -1964,15 +2005,13 @@ set_control_mode() } void -print_reject_mode(struct vehicle_status_s *status, const char *msg) +print_reject_mode(struct vehicle_status_s *status_local, 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: REJECT %s", msg); - mavlink_log_critical(mavlink_fd, s); + mavlink_log_critical(mavlink_fd, "REJECT %s", msg); /* only buzz if armed, because else we're driving people nuts indoors they really need to look at the leds as well. */ @@ -1987,9 +2026,7 @@ print_reject_arm(const char *msg) if (t - last_print_mode_reject_time > PRINT_MODE_REJECT_INTERVAL) { last_print_mode_reject_time = t; - char s[80]; - sprintf(s, "#audio: %s", msg); - mavlink_log_critical(mavlink_fd, s); + mavlink_log_critical(mavlink_fd, msg); tune_negative(true); } } @@ -2002,12 +2039,12 @@ void answer_command(struct vehicle_command_s &cmd, enum VEHICLE_CMD_RESULT resul break; case VEHICLE_CMD_RESULT_DENIED: - mavlink_log_critical(mavlink_fd, "#audio: command denied: %u", cmd.command); + mavlink_log_critical(mavlink_fd, "command denied: %u", cmd.command); tune_negative(true); break; case VEHICLE_CMD_RESULT_FAILED: - mavlink_log_critical(mavlink_fd, "#audio: command failed: %u", cmd.command); + mavlink_log_critical(mavlink_fd, "command failed: %u", cmd.command); tune_negative(true); break; @@ -2018,7 +2055,7 @@ void answer_command(struct vehicle_command_s &cmd, enum VEHICLE_CMD_RESULT resul break; case VEHICLE_CMD_RESULT_UNSUPPORTED: - mavlink_log_critical(mavlink_fd, "#audio: command unsupported: %u", cmd.command); + mavlink_log_critical(mavlink_fd, "command unsupported: %u", cmd.command); tune_negative(true); break; diff --git a/src/modules/commander/commander_helper.cpp b/src/modules/commander/commander_helper.cpp index 80e6861f6..d5fe122cb 100644 --- a/src/modules/commander/commander_helper.cpp +++ b/src/modules/commander/commander_helper.cpp @@ -1,9 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. - * Author: Thomas Gubler <thomasgubler@student.ethz.ch> - * Julian Oes <joes@student.ethz.ch> - * Anton Babushkin <anton.babushkin@me.com> + * Copyright (c) 2013, 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 @@ -37,6 +34,11 @@ /** * @file commander_helper.cpp * Commander helper functions implementations + * + * @author Thomas Gubler <thomasgubler@student.ethz.ch> + * @author Julian Oes <julian@oes.ch> + * @author Anton Babushkin <anton.babushkin@me.com> + * */ #include <stdio.h> diff --git a/src/modules/commander/commander_helper.h b/src/modules/commander/commander_helper.h index e75f2592f..a49c9e263 100644 --- a/src/modules/commander/commander_helper.h +++ b/src/modules/commander/commander_helper.h @@ -1,8 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. - * Author: Thomas Gubler <thomasgubler@student.ethz.ch> - * Julian Oes <joes@student.ethz.ch> + * Copyright (c) 2013, 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 @@ -36,6 +34,9 @@ /** * @file commander_helper.h * Commander helper functions definitions + * + * @author Thomas Gubler <thomasgubler@student.ethz.ch> + * @author Julian Oes <julian@oes.ch> */ #ifndef COMMANDER_HELPER_H_ @@ -77,6 +78,8 @@ void rgbled_set_pattern(rgbled_pattern_t *pattern); * Use integral of current if battery capacity known (BAT_CAPACITY parameter set), * else use simple estimate based on voltage. * + * @param voltage the current battery voltage + * @param discharged the discharged capacity * @return the estimated remaining capacity in 0..1 */ float battery_remaining_estimate_voltage(float voltage, float discharged); diff --git a/src/modules/commander/mag_calibration.h b/src/modules/commander/mag_calibration.h index a101cd7b1..c14f948cc 100644 --- a/src/modules/commander/mag_calibration.h +++ b/src/modules/commander/mag_calibration.h @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * Copyright (c) 2013, 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 diff --git a/src/modules/commander/state_machine_helper.cpp b/src/modules/commander/state_machine_helper.cpp index 6b96e3a3f..372ba9d7d 100644 --- a/src/modules/commander/state_machine_helper.cpp +++ b/src/modules/commander/state_machine_helper.cpp @@ -52,6 +52,7 @@ #include <uORB/topics/vehicle_status.h> #include <uORB/topics/actuator_controls.h> #include <uORB/topics/differential_pressure.h> +#include <uORB/topics/airspeed.h> #include <systemlib/systemlib.h> #include <systemlib/param/param.h> #include <systemlib/err.h> @@ -70,8 +71,6 @@ #endif static const int ERROR = -1; -static int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd); - // This array defines the arming state transitions. The rows are the new state, and the columns // are the current state. Using new state and current state you can index into the array which // will be true for a valid transition or false for a invalid transition. In some cases even @@ -89,7 +88,7 @@ static const bool arming_transitions[ARMING_STATE_MAX][ARMING_STATE_MAX] = { }; // You can index into the array with an arming_state_t in order to get it's textual representation -static const char *state_names[ARMING_STATE_MAX] = { +static const char * const state_names[ARMING_STATE_MAX] = { "ARMING_STATE_INIT", "ARMING_STATE_STANDBY", "ARMING_STATE_ARMED", @@ -162,7 +161,7 @@ arming_state_transition(struct vehicle_status_s *status, /// current // Fail transition if we need safety switch press } else if (safety->safety_switch_available && !safety->safety_off) { - mavlink_log_critical(mavlink_fd, "#audio: NOT ARMING: Press safety switch!"); + mavlink_log_critical(mavlink_fd, "NOT ARMING: Press safety switch!"); valid_transition = false; } @@ -173,16 +172,16 @@ arming_state_transition(struct vehicle_status_s *status, /// current // Fail transition if power is not good if (!status->condition_power_input_valid) { - mavlink_log_critical(mavlink_fd, "#audio: NOT ARMING: Connect power module."); + mavlink_log_critical(mavlink_fd, "NOT ARMING: Connect power module."); valid_transition = false; } // Fail transition if power levels on the avionics rail // are measured but are insufficient - if (status->condition_power_input_valid && (status->avionics_power_rail_voltage > 0.0f) && - (status->avionics_power_rail_voltage < 4.9f)) { + if (status->condition_power_input_valid && ((status->avionics_power_rail_voltage > 0.0f) && + (status->avionics_power_rail_voltage < 4.9f))) { - mavlink_log_critical(mavlink_fd, "#audio: NOT ARMING: Avionics power low: %6.2f V.", (double)status->avionics_power_rail_voltage); + mavlink_log_critical(mavlink_fd, "NOT ARMING: Avionics power low: %6.2f V.", (double)status->avionics_power_rail_voltage); valid_transition = false; } } @@ -622,19 +621,21 @@ bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_en int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) { int ret; + bool failed = false; int fd = open(ACCEL_DEVICE_PATH, O_RDONLY); if (fd < 0) { - mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL SENSOR MISSING"); - ret = fd; + mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL SENSOR MISSING"); + failed = true; goto system_eval; } ret = ioctl(fd, ACCELIOCSELFTEST, 0); if (ret != OK) { - mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL CALIBRATION"); + mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL CALIBRATION"); + failed = true; goto system_eval; } @@ -644,55 +645,43 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) if (ret == sizeof(acc)) { /* evaluate values */ - float accel_scale = sqrtf(acc.x * acc.x + acc.y * acc.y + acc.z * acc.z); - - if (accel_scale < 9.78f || accel_scale > 9.83f) { - mavlink_log_info(mavlink_fd, "#audio: Accelerometer calibration recommended."); - } + float accel_magnitude = sqrtf(acc.x * acc.x + acc.y * acc.y + acc.z * acc.z); - if (accel_scale > 30.0f /* m/s^2 */) { - mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL RANGE"); + if (accel_magnitude < 4.0f || accel_magnitude > 15.0f /* m/s^2 */) { + mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL RANGE"); + mavlink_log_critical(mavlink_fd, "hold still while arming"); /* this is frickin' fatal */ - ret = ERROR; + failed = true; goto system_eval; - } else { - ret = OK; } } else { - mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL READ"); + mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL READ"); /* this is frickin' fatal */ - ret = ERROR; + failed = true; goto system_eval; } if (!status->is_rotary_wing) { - fd = open(AIRSPEED_DEVICE_PATH, O_RDONLY); + /* accel done, close it */ + close(fd); + fd = orb_subscribe(ORB_ID(airspeed)); + + struct airspeed_s airspeed; - if (fd < 0) { - mavlink_log_critical(mavlink_fd, "#audio: FAIL: AIRSPEED SENSOR MISSING"); - ret = fd; + if ((ret = orb_copy(ORB_ID(airspeed), fd, &airspeed)) || + (hrt_elapsed_time(&airspeed.timestamp) > (50 * 1000))) { + mavlink_log_critical(mavlink_fd, "ARM FAIL: AIRSPEED SENSOR MISSING"); + failed = true; goto system_eval; } - struct differential_pressure_s diff_pres; - - ret = read(fd, &diff_pres, sizeof(diff_pres)); - - if (ret == sizeof(diff_pres)) { - if (fabsf(diff_pres.differential_pressure_filtered_pa > 5.0f)) { - mavlink_log_critical(mavlink_fd, "#audio: WARNING AIRSPEED CALIBRATION MISSING"); - // XXX do not make this fatal yet - ret = OK; - } - } else { - mavlink_log_critical(mavlink_fd, "#audio: FAIL: AIRSPEED READ"); - /* this is frickin' fatal */ - ret = ERROR; - goto system_eval; + if (fabsf(airspeed.indicated_airspeed_m_s > 6.0f)) { + mavlink_log_critical(mavlink_fd, "AIRSPEED WARNING: WIND OR CALIBRATION MISSING"); + // XXX do not make this fatal yet } } system_eval: close(fd); - return ret; + return (failed); } diff --git a/src/modules/commander/state_machine_helper.h b/src/modules/commander/state_machine_helper.h index 11072403e..bb1b87e71 100644 --- a/src/modules/commander/state_machine_helper.h +++ b/src/modules/commander/state_machine_helper.h @@ -1,8 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. - * Author: Thomas Gubler <thomasgubler@student.ethz.ch> - * Julian Oes <joes@student.ethz.ch> + * Copyright (c) 2013, 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 @@ -36,14 +34,14 @@ /** * @file state_machine_helper.h * State machine helper functions definitions + * + * @author Thomas Gubler <thomasgubler@student.ethz.ch> + * @author Julian Oes <julian@oes.ch> */ #ifndef STATE_MACHINE_HELPER_H_ #define STATE_MACHINE_HELPER_H_ -#define GPS_NOFIX_COUNTER_LIMIT 4 //need GPS_NOFIX_COUNTER_LIMIT gps packets with a bad fix to call an error (if outdoor) -#define GPS_GOTFIX_COUNTER_REQUIRED 4 //need GPS_GOTFIX_COUNTER_REQUIRED gps packets with a good fix to obtain position lock - #include <uORB/uORB.h> #include <uORB/topics/vehicle_status.h> #include <uORB/topics/actuator_armed.h> @@ -67,4 +65,6 @@ transition_result_t hil_state_transition(hil_state_t new_state, int status_pub, bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_enabled, const bool mission_finished); +int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd); + #endif /* STATE_MACHINE_HELPER_H_ */ |