/**************************************************************************** * * Copyright (c) 2017 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 * are met: * * 1. Redistributions of source code must retain the above copyright * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE * POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************/ #ifndef COMMANDER_HPP_ #define COMMANDER_HPP_ #include "state_machine_helper.h" #include "failure_detector/FailureDetector.hpp" #include #include #include #include // publications #include #include #include #include #include #include #include #include // subscriptions #include #include #include #include #include #include #include #include using math::constrain; using uORB::Publication; using uORB::Subscription; using namespace time_literals; class Commander : public ModuleBase, public ModuleParams { public: Commander(); /** @see ModuleBase */ static int task_spawn(int argc, char *argv[]); /** @see ModuleBase */ static Commander *instantiate(int argc, char *argv[]); /** @see ModuleBase */ static int custom_command(int argc, char *argv[]); /** @see ModuleBase */ static int print_usage(const char *reason = nullptr); /** @see ModuleBase::run() */ void run() override; void enable_hil(); // TODO: only temporarily static until low priority thread is removed static bool preflight_check(bool report); private: DEFINE_PARAMETERS( (ParamFloat) _home_eph_threshold, (ParamFloat) _home_epv_threshold, (ParamFloat) _eph_threshold, (ParamFloat) _epv_threshold, (ParamFloat) _evh_threshold, (ParamInt) _failsafe_pos_delay, (ParamInt) _failsafe_pos_probation, (ParamInt) _failsafe_pos_gain, (ParamInt) _low_bat_action ) const int64_t POSVEL_PROBATION_MIN = 1_s; /**< minimum probation duration (usec) */ const int64_t POSVEL_PROBATION_MAX = 100_s; /**< maximum probation duration (usec) */ hrt_abstime _last_gpos_fail_time_us{0}; /**< Last time that the global position validity recovery check failed (usec) */ hrt_abstime _last_lpos_fail_time_us{0}; /**< Last time that the local position validity recovery check failed (usec) */ hrt_abstime _last_lvel_fail_time_us{0}; /**< Last time that the local velocity validity recovery check failed (usec) */ // Probation times for position and velocity validity checks to pass if failed hrt_abstime _gpos_probation_time_us = POSVEL_PROBATION_MIN; hrt_abstime _lpos_probation_time_us = POSVEL_PROBATION_MIN; hrt_abstime _lvel_probation_time_us = POSVEL_PROBATION_MIN; /* class variables used to check for navigation failure after takeoff */ hrt_abstime _time_at_takeoff{0}; /**< last time we were on the ground */ hrt_abstime _time_last_innov_pass{0}; /**< last time velocity innovations passed */ bool _nav_test_passed{false}; /**< true if the post takeoff navigation test has passed */ bool _nav_test_failed{false}; /**< true if the post takeoff navigation test has failed */ FailureDetector _failure_detector; bool _failure_detector_termination_printed{false}; bool handle_command(vehicle_status_s *status, const vehicle_command_s &cmd, actuator_armed_s *armed, home_position_s *home, orb_advert_t *home_pub, orb_advert_t *command_ack_pub, bool *changed); bool set_home_position(orb_advert_t &homePub, home_position_s &home, bool set_alt_only_to_lpos_ref); // Set the main system state based on RC and override device inputs transition_result_t set_main_state(const vehicle_status_s &status, bool *changed); // Enable override (manual reversion mode) on the system transition_result_t set_main_state_override_on(const vehicle_status_s &status, bool *changed); // Set the system main state based on the current RC inputs transition_result_t set_main_state_rc(const vehicle_status_s &status, bool *changed); void check_valid(const hrt_abstime ×tamp, const hrt_abstime &timeout, const bool valid_in, bool *valid_out, bool *changed); bool check_posvel_validity(const bool data_valid, const float data_accuracy, const float required_accuracy, const hrt_abstime &data_timestamp_us, hrt_abstime *last_fail_time_us, hrt_abstime *probation_time_us, bool *valid_state, bool *validity_changed); void reset_posvel_validity(bool *changed); void mission_init(); /** * Update the telemetry status and the corresponding status variables. * Perform system checks when new telemetry link connected. */ void poll_telemetry_status(); /** * Checks the status of all available data links and handles switching between different system telemetry states. */ void data_link_checks(int32_t highlatencydatalink_loss_timeout, int32_t highlatencydatalink_regain_timeout, int32_t datalink_loss_timeout, int32_t datalink_regain_timeout, bool *status_changed); // telemetry variables struct telemetry_data { int subscriber = -1; uint64_t last_heartbeat = 0u; uint64_t last_dl_loss = 0u; bool preflight_checks_reported = false; bool lost = true; bool high_latency = false; } _telemetry[ORB_MULTI_MAX_INSTANCES]; void estimator_check(bool *status_changed); int _battery_sub{-1}; uint8_t _battery_warning{battery_status_s::BATTERY_WARNING_NONE}; float _battery_current{0.0f}; void battery_status_check(); // Subscriptions Subscription _estimator_status_sub{ORB_ID(estimator_status)}; Subscription _iridiumsbd_status_sub{ORB_ID(iridiumsbd_status)}; Subscription _mission_result_sub{ORB_ID(mission_result)}; Subscription _global_position_sub{ORB_ID(vehicle_global_position)}; Subscription _local_position_sub{ORB_ID(vehicle_local_position)}; }; #endif /* COMMANDER_HPP_ */