diff options
Diffstat (limited to 'src/modules/commander/state_machine_helper.cpp')
-rw-r--r-- | src/modules/commander/state_machine_helper.cpp | 169 |
1 files changed, 149 insertions, 20 deletions
diff --git a/src/modules/commander/state_machine_helper.cpp b/src/modules/commander/state_machine_helper.cpp index 4339a7a76..210a118f6 100644 --- a/src/modules/commander/state_machine_helper.cpp +++ b/src/modules/commander/state_machine_helper.cpp @@ -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 @@ -46,20 +46,32 @@ #include <dirent.h> #include <fcntl.h> #include <string.h> +#include <math.h> #include <uORB/uORB.h> #include <uORB/topics/vehicle_status.h> #include <uORB/topics/actuator_controls.h> +#include <uORB/topics/differential_pressure.h> #include <systemlib/systemlib.h> #include <systemlib/param/param.h> #include <systemlib/err.h> #include <drivers/drv_hrt.h> +#include <drivers/drv_accel.h> +#include <drivers/drv_airspeed.h> #include <drivers/drv_device.h> #include <mavlink/mavlink_log.h> #include "state_machine_helper.h" #include "commander_helper.h" +/* oddly, ERROR is not defined for c++ */ +#ifdef ERROR +# undef ERROR +#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 @@ -98,18 +110,31 @@ arming_state_transition(struct vehicle_status_s *status, /// current ASSERT(ARMING_STATE_INIT == 0); ASSERT(ARMING_STATE_IN_AIR_RESTORE == ARMING_STATE_MAX - 1); - /* - * Perform an atomic state update - */ - irqstate_t flags = irqsave(); - transition_result_t ret = TRANSITION_DENIED; + arming_state_t current_arming_state = status->arming_state; + /* only check transition if the new state is actually different from the current one */ - if (new_arming_state == status->arming_state) { + if (new_arming_state == current_arming_state) { ret = TRANSITION_NOT_CHANGED; } else { + + /* + * Get sensing state if necessary + */ + int prearm_ret = OK; + + /* only perform the check if we have to */ + if (new_arming_state == ARMING_STATE_ARMED) { + prearm_ret = prearm_check(status, mavlink_fd); + } + + /* + * Perform an atomic state update + */ + irqstate_t flags = irqsave(); + /* enforce lockdown in HIL */ if (status->hil_state == HIL_STATE_ON) { armed->lockdown = true; @@ -124,15 +149,44 @@ arming_state_transition(struct vehicle_status_s *status, /// current if (valid_transition) { // We have a good transition. Now perform any secondary validation. if (new_arming_state == ARMING_STATE_ARMED) { - // Fail transition if we need safety switch press - // Allow if coming from in air restore + + // Do not perform pre-arm checks if coming from in air restore // Allow if HIL_STATE_ON - if (status->arming_state != ARMING_STATE_IN_AIR_RESTORE && status->hil_state == HIL_STATE_OFF && safety->safety_switch_available && !safety->safety_off) { - if (mavlink_fd) { - mavlink_log_critical(mavlink_fd, "#audio: NOT ARMING: Press safety switch first."); + if (status->arming_state != ARMING_STATE_IN_AIR_RESTORE && + status->hil_state == HIL_STATE_OFF) { + + // Fail transition if pre-arm check fails + if (prearm_ret) { + valid_transition = false; + + // 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!"); + + valid_transition = false; + } + + // Perform power checks only if circuit breaker is not + // engaged for these checks + if (!status->circuit_breaker_engaged_power_check) { + // Fail transition if power is not good + if (!status->condition_power_input_valid) { + + mavlink_log_critical(mavlink_fd, "#audio: 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)) { + + mavlink_log_critical(mavlink_fd, "#audio: NOT ARMING: Avionics power low: %6.2f V.", (double)status->avionics_power_rail_voltage); + valid_transition = false; + } } - valid_transition = false; } } else if (new_arming_state == ARMING_STATE_STANDBY && status->arming_state == ARMING_STATE_ARMED_ERROR) { @@ -157,17 +211,15 @@ arming_state_transition(struct vehicle_status_s *status, /// current ret = TRANSITION_CHANGED; status->arming_state = new_arming_state; } - } - /* end of atomic state update */ - irqrestore(flags); + /* end of atomic state update */ + irqrestore(flags); + } if (ret == TRANSITION_DENIED) { - static const char *errMsg = "Invalid arming transition from %s to %s"; + static const char *errMsg = "INVAL: %s - %s"; - if (mavlink_fd) { - mavlink_log_critical(mavlink_fd, errMsg, state_names[status->arming_state], state_names[new_arming_state]); - } + mavlink_log_critical(mavlink_fd, errMsg, state_names[status->arming_state], state_names[new_arming_state]); warnx(errMsg, state_names[status->arming_state], state_names[new_arming_state]); } @@ -567,3 +619,80 @@ bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_en return status->nav_state != nav_state_old; } +int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) +{ + int ret; + + int fd = open(ACCEL_DEVICE_PATH, O_RDONLY); + + if (fd < 0) { + mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL SENSOR MISSING"); + ret = fd; + goto system_eval; + } + + ret = ioctl(fd, ACCELIOCSELFTEST, 0); + + if (ret != OK) { + mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL CALIBRATION"); + goto system_eval; + } + + /* check measurement result range */ + struct accel_report acc; + ret = read(fd, &acc, sizeof(acc)); + + 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."); + } + + if (accel_scale > 30.0f /* m/s^2 */) { + mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL RANGE"); + /* this is frickin' fatal */ + ret = ERROR; + goto system_eval; + } else { + ret = OK; + } + } else { + mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL READ"); + /* this is frickin' fatal */ + ret = ERROR; + goto system_eval; + } + + if (!status->is_rotary_wing) { + fd = open(AIRSPEED_DEVICE_PATH, O_RDONLY); + + if (fd < 0) { + mavlink_log_critical(mavlink_fd, "#audio: FAIL: AIRSPEED SENSOR MISSING"); + ret = fd; + 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; + } + } + +system_eval: + close(fd); + return ret; +} |