diff options
author | Lorenz Meier <lm@inf.ethz.ch> | 2014-07-13 12:46:49 +0200 |
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committer | Lorenz Meier <lm@inf.ethz.ch> | 2014-07-13 12:46:49 +0200 |
commit | 91651bf240e0b2f53936f45d59ffae2c970eac9c (patch) | |
tree | 5ceadc4a54f50545b529d0af6480ba37e972b259 /src/modules | |
parent | 8590d555b432f206e2b88893ea5198c1398aa99c (diff) | |
parent | a32577377b8d735c77ffaaee15e2bbfa74be703f (diff) | |
download | px4-firmware-91651bf240e0b2f53936f45d59ffae2c970eac9c.tar.gz px4-firmware-91651bf240e0b2f53936f45d59ffae2c970eac9c.tar.bz2 px4-firmware-91651bf240e0b2f53936f45d59ffae2c970eac9c.zip |
Merged commander fixes into airspeed_test_fix
Diffstat (limited to 'src/modules')
-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.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 | 182 | ||||
-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 | 26 | ||||
-rw-r--r-- | src/modules/commander/state_machine_helper.h | 10 | ||||
-rw-r--r-- | src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp | 125 | ||||
-rw-r--r-- | src/modules/ekf_att_pos_estimator/estimator_23states.cpp | 16 |
16 files changed, 191 insertions, 210 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.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 e14dff197..0c4d48dea 100644 --- a/src/modules/commander/commander.cpp +++ b/src/modules/commander/commander.cpp @@ -403,10 +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; } @@ -425,7 +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"); @@ -434,43 +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); } } } @@ -485,22 +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 { @@ -512,20 +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, @@ -543,7 +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; @@ -561,7 +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; @@ -598,7 +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; @@ -688,11 +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); @@ -766,8 +775,9 @@ int commander_thread_main(int argc, char *argv[]) mavlink_log_info(mavlink_fd, "[cmd] dataman_id=%d, count=%u, current=%d", mission.dataman_id, mission.count, mission.current_seq); } else { - warnx("reading mission state failed"); - mavlink_log_info(mavlink_fd, "[cmd] reading mission state failed"); + const char *missionfail = "reading mission state failed"; + warnx("%s", missionfail); + mavlink_log_critical(mavlink_fd, missionfail); /* initialize mission state in dataman */ mission.dataman_id = 0; @@ -780,8 +790,6 @@ int commander_thread_main(int argc, char *argv[]) orb_publish(ORB_ID(offboard_mission), mission_pub, &mission); } - mavlink_log_info(mavlink_fd, "[cmd] started"); - int ret; pthread_attr_t commander_low_prio_attr; @@ -1074,7 +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; } } @@ -1178,10 +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"); } } } @@ -1261,14 +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) { @@ -1330,12 +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; } } @@ -1376,7 +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) { @@ -1396,16 +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); } @@ -1419,12 +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; } @@ -1436,14 +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; } } @@ -1458,7 +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; } @@ -1642,22 +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; @@ -1668,12 +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 { @@ -1706,7 +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); } @@ -1719,16 +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; @@ -1743,78 +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 @@ -1822,21 +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; @@ -2001,15 +2009,13 @@ 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. */ @@ -2024,9 +2030,7 @@ 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); } } @@ -2039,12 +2043,12 @@ 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; @@ -2055,7 +2059,7 @@ 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 e90c77af4..09ea12c38 100644 --- a/src/modules/commander/state_machine_helper.cpp +++ b/src/modules/commander/state_machine_helper.cpp @@ -88,7 +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", @@ -161,7 +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; } @@ -172,16 +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; } } @@ -626,7 +626,7 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) int fd = open(ACCEL_DEVICE_PATH, O_RDONLY); if (fd < 0) { - mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL SENSOR MISSING"); + mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL SENSOR MISSING"); failed = true; goto system_eval; } @@ -634,7 +634,7 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) 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; } @@ -648,14 +648,14 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) float accel_magnitude = sqrtf(acc.x * acc.x + acc.y * acc.y + acc.z * acc.z); if (accel_magnitude < 4.0f || accel_magnitude > 15.0f /* m/s^2 */) { - mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL RANGE"); - mavlink_log_info(mavlink_fd, "#audio: hold still while arming"); + mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL RANGE"); + mavlink_log_critical(mavlink_fd, "hold still while arming"); /* this is frickin' fatal */ failed = true; goto system_eval; } } else { - mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL READ"); + mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL READ"); /* this is frickin' fatal */ failed = true; goto system_eval; @@ -670,13 +670,13 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) if (ret = orb_copy(ORB_ID(airspeed), fd, &airspeed) || hrt_elapsed_time(&airspeed.timestamp) > 50 * 1000) { - mavlink_log_critical(mavlink_fd, "#audio: FAIL: AIRSPEED SENSOR MISSING"); + mavlink_log_critical(mavlink_fd, "ARM FAIL: AIRSPEED SENSOR MISSING"); failed = true; goto system_eval; } if (fabsf(airspeed.indicated_airspeed_m_s > 6.0f)) { - mavlink_log_critical(mavlink_fd, "#audio: WIND OR CALIBRATION MISSING"); + mavlink_log_critical(mavlink_fd, "AIRSPEED WARNING: WIND OR CALIBRATION MISSING"); // XXX do not make this fatal yet } } diff --git a/src/modules/commander/state_machine_helper.h b/src/modules/commander/state_machine_helper.h index ddc5bf154..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> diff --git a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp index 5d768b73d..ee1561280 100644 --- a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp +++ b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp @@ -559,61 +559,26 @@ FixedwingEstimator::check_filter_state() int check = _ekf->CheckAndBound(&ekf_report); - const char* ekfname = "att pos estimator: "; - - switch (check) { - case 0: - /* all ok */ - break; - case 1: - { - const char* str = "NaN in states, resetting"; - warnx("%s", str); - mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); - break; - } - case 2: - { - const char* str = "stale IMU data, resetting"; - warnx("%s", str); - mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); - break; - } - case 3: - { - const char* str = "switching to dynamic state"; - warnx("%s", str); - mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); - break; - } - case 4: - { - const char* str = "excessive gyro offsets"; - warnx("%s", str); - mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); - break; - } - case 5: - { - const char* str = "GPS velocity divergence"; - warnx("%s", str); - mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); - break; - } - case 6: - { - const char* str = "excessive covariances"; - warnx("%s", str); - mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); - break; + const char* const feedback[] = { 0, + "NaN in states, resetting", + "stale IMU data, resetting", + "got initial position lock", + "excessive gyro offsets", + "GPS velocity divergence", + "excessive covariances", + "unknown condition"}; + + // Print out error condition + if (check) { + unsigned warn_index = static_cast<unsigned>(check); + unsigned max_warn_index = (sizeof(feedback) / sizeof(feedback[0])); + + if (max_warn_index < warn_index) { + warn_index = max_warn_index; } - default: - { - const char* str = "unknown reset condition"; - warnx("%s", str); - mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); - } + warnx("reset: %s", feedback[warn_index]); + mavlink_log_critical(_mavlink_fd, "[ekf] re-init: %s", feedback[warn_index]); } struct estimator_status_report rep; @@ -645,6 +610,10 @@ FixedwingEstimator::check_filter_state() rep.health_flags |= (((uint8_t)ekf_report.posHealth) << 1); rep.health_flags |= (((uint8_t)ekf_report.hgtHealth) << 2); rep.health_flags |= (((uint8_t)!ekf_report.gyroOffsetsExcessive) << 3); + // rep.health_flags |= (((uint8_t)ekf_report.onGround) << 4); + // rep.health_flags |= (((uint8_t)ekf_report.staticMode) << 5); + // rep.health_flags |= (((uint8_t)ekf_report.useCompass) << 6); + // rep.health_flags |= (((uint8_t)ekf_report.useAirspeed) << 7); rep.timeout_flags |= (((uint8_t)ekf_report.velTimeout) << 0); rep.timeout_flags |= (((uint8_t)ekf_report.posTimeout) << 1); @@ -1202,10 +1171,10 @@ FixedwingEstimator::task_main() _baro_gps_offset = 0.0f; _ekf->InitialiseFilter(initVelNED, 0.0, 0.0, 0.0f, 0.0f); + } else if (_ekf->statesInitialised) { // We're apparently initialized in this case now - int check = check_filter_state(); if (check) { @@ -1213,7 +1182,6 @@ FixedwingEstimator::task_main() continue; } - // Run the strapdown INS equations every IMU update _ekf->UpdateStrapdownEquationsNED(); #if 0 @@ -1281,7 +1249,11 @@ FixedwingEstimator::task_main() // run the fusion step _ekf->FuseVelposNED(); - } else if (_ekf->statesInitialised) { + } else if (!_gps_initialized) { + + // force static mode + _ekf->staticMode = true; + // Convert GPS measurements to Pos NE, hgt and Vel NED _ekf->velNED[0] = 0.0f; _ekf->velNED[1] = 0.0f; @@ -1303,7 +1275,7 @@ FixedwingEstimator::task_main() _ekf->fusePosData = false; } - if (newHgtData && _ekf->statesInitialised) { + if (newHgtData) { // Could use a blend of GPS and baro alt data if desired _ekf->hgtMea = 1.0f * (_ekf->baroHgt - _baro_ref); _ekf->fuseHgtData = true; @@ -1317,7 +1289,7 @@ FixedwingEstimator::task_main() } // Fuse Magnetometer Measurements - if (newDataMag && _ekf->statesInitialised) { + if (newDataMag) { _ekf->fuseMagData = true; _ekf->RecallStates(_ekf->statesAtMagMeasTime, (IMUmsec - _parameters.mag_delay_ms)); // Assume 50 msec avg delay for magnetometer data @@ -1331,7 +1303,7 @@ FixedwingEstimator::task_main() } // Fuse Airspeed Measurements - if (newAdsData && _ekf->statesInitialised && _ekf->VtasMeas > 8.0f) { + if (newAdsData && _ekf->VtasMeas > 7.0f) { _ekf->fuseVtasData = true; _ekf->RecallStates(_ekf->statesAtVtasMeasTime, (IMUmsec - _parameters.tas_delay_ms)); // assume 100 msec avg delay for airspeed data _ekf->FuseAirspeed(); @@ -1399,7 +1371,7 @@ FixedwingEstimator::task_main() _velocity_xy_filtered = 0.95f*_velocity_xy_filtered + 0.05f*sqrtf(_local_pos.vx*_local_pos.vx + _local_pos.vy*_local_pos.vy); _velocity_z_filtered = 0.95f*_velocity_z_filtered + 0.05f*fabsf(_local_pos.vz); - _airspeed_filtered = 0.95f*_airspeed_filtered + + 0.05f*_airspeed.true_airspeed_m_s; + _airspeed_filtered = 0.95f*_airspeed_filtered + 0.05f*_airspeed.true_airspeed_m_s; /* crude land detector for fixedwing only, @@ -1490,27 +1462,28 @@ FixedwingEstimator::task_main() } - } - - } + if (hrt_elapsed_time(&_wind.timestamp) > 99000) { + _wind.timestamp = _global_pos.timestamp; + _wind.windspeed_north = _ekf->states[14]; + _wind.windspeed_east = _ekf->states[15]; + _wind.covariance_north = _ekf->P[14][14]; + _wind.covariance_east = _ekf->P[15][15]; - if (hrt_elapsed_time(&_wind.timestamp) > 99000) { - _wind.timestamp = _global_pos.timestamp; - _wind.windspeed_north = _ekf->states[14]; - _wind.windspeed_east = _ekf->states[15]; - _wind.covariance_north = _ekf->P[14][14]; - _wind.covariance_east = _ekf->P[15][15]; + /* lazily publish the wind estimate only once available */ + if (_wind_pub > 0) { + /* publish the wind estimate */ + orb_publish(ORB_ID(wind_estimate), _wind_pub, &_wind); - /* lazily publish the wind estimate only once available */ - if (_wind_pub > 0) { - /* publish the wind estimate */ - orb_publish(ORB_ID(wind_estimate), _wind_pub, &_wind); + } else { + /* advertise and publish */ + _wind_pub = orb_advertise(ORB_ID(wind_estimate), &_wind); + } + } - } else { - /* advertise and publish */ - _wind_pub = orb_advertise(ORB_ID(wind_estimate), &_wind); } + } + } } diff --git a/src/modules/ekf_att_pos_estimator/estimator_23states.cpp b/src/modules/ekf_att_pos_estimator/estimator_23states.cpp index f33a1d780..e83c37bbd 100644 --- a/src/modules/ekf_att_pos_estimator/estimator_23states.cpp +++ b/src/modules/ekf_att_pos_estimator/estimator_23states.cpp @@ -2206,7 +2206,7 @@ void AttPosEKF::calcLLH(float posNED[3], double &lat, double &lon, float &hgt, d void AttPosEKF::OnGroundCheck() { - onGround = (((sq(velNED[0]) + sq(velNED[1]) + sq(velNED[2])) < 4.0f) && (VtasMeas < 6.0f)); + onGround = (((sq(velNED[0]) + sq(velNED[1]) + sq(velNED[2])) < 4.0f) && (VtasMeas < 8.0f)); if (staticMode) { staticMode = (!refSet || (GPSstatus < GPS_FIX_3D)); } @@ -2806,12 +2806,18 @@ void AttPosEKF::InitializeDynamic(float (&initvelNED)[3], float declination) current_ekf_state.statesNaN = false; current_ekf_state.velHealth = true; - //current_ekf_state.posHealth = ?; - //current_ekf_state.hgtHealth = ?; + current_ekf_state.posHealth = true; + current_ekf_state.hgtHealth = true; current_ekf_state.velTimeout = false; - //current_ekf_state.posTimeout = ?; - //current_ekf_state.hgtTimeout = ?; + current_ekf_state.posTimeout = false; + current_ekf_state.hgtTimeout = false; + + fuseVelData = false; + fusePosData = false; + fuseHgtData = false; + fuseMagData = false; + fuseVtasData = false; // Fill variables with valid data velNED[0] = initvelNED[0]; |