5 changed files with 551 additions and 2 deletions
@ -0,0 +1,456 @@
@@ -0,0 +1,456 @@
|
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/****************************************************************************
|
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* |
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* Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. |
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* |
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* Redistribution and use in source and binary forms, with or without |
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* modification, are permitted provided that the following conditions |
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* are met: |
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* |
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* 1. Redistributions of source code must retain the above copyright |
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* notice, this list of conditions and the following disclaimer. |
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* 2. Redistributions in binary form must reproduce the above copyright |
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* notice, this list of conditions and the following disclaimer in |
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* the documentation and/or other materials provided with the |
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* distribution. |
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* 3. Neither the name PX4 nor the names of its contributors may be |
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* used to endorse or promote products derived from this software |
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* without specific prior written permission. |
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* |
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS |
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT |
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS |
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE |
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, |
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, |
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS |
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED |
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT |
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN |
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
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* POSSIBILITY OF SUCH DAMAGE. |
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* |
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****************************************************************************/ |
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/**
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* @file fw_att_pos_estimator_main.cpp |
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* Implementation of the attitude and position estimator. |
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* |
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*/ |
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#include <nuttx/config.h> |
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#include <stdio.h> |
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#include <stdlib.h> |
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#include <string.h> |
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#include <unistd.h> |
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#include <fcntl.h> |
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#include <errno.h> |
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#include <math.h> |
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#include <poll.h> |
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#include <time.h> |
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#include <drivers/drv_hrt.h> |
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#include <drivers/drv_gyro.h> |
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#include <drivers/drv_accel.h> |
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#include <drivers/drv_mag.h> |
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#include <arch/board/board.h> |
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#include <uORB/uORB.h> |
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#include <uORB/topics/airspeed.h> |
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#include <uORB/topics/vehicle_global_position.h> |
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#include <uORB/topics/vehicle_attitude.h> |
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#include <uORB/topics/vehicle_attitude_setpoint.h> |
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#include <uORB/topics/manual_control_setpoint.h> |
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#include <uORB/topics/actuator_controls.h> |
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#include <uORB/topics/vehicle_rates_setpoint.h> |
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#include <uORB/topics/vehicle_attitude.h> |
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#include <uORB/topics/vehicle_status.h> |
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#include <uORB/topics/parameter_update.h> |
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#include <uORB/topics/mission.h> |
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#include <systemlib/param/param.h> |
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#include <systemlib/err.h> |
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#include <geo/geo.h> |
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#include <systemlib/perf_counter.h> |
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#include <systemlib/systemlib.h> |
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#include <mathlib/mathlib.h> |
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/**
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* estimator app start / stop handling function |
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* |
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* @ingroup apps |
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*/ |
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extern "C" __EXPORT int fw_att_pos_estimator_main(int argc, char *argv[]); |
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class FixedwingEstimator |
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{ |
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public: |
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/**
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* Constructor |
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*/ |
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FixedwingEstimator(); |
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/**
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* Destructor, also kills the sensors task. |
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*/ |
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~FixedwingEstimator(); |
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/**
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* Start the sensors task. |
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* |
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* @return OK on success. |
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*/ |
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int start(); |
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private: |
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bool _task_should_exit; /**< if true, sensor task should exit */ |
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int _estimator_task; /**< task handle for sensor task */ |
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int _global_pos_sub; |
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int _gyro_sub; /**< gyro sensor subscription */ |
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int _accel_sub; /**< accel sensor subscription */ |
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int _mag_sub; /**< mag sensor subscription */ |
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int _attitude_sub; /**< raw rc channels data subscription */ |
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int _airspeed_sub; /**< airspeed subscription */ |
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int _vstatus_sub; /**< vehicle status subscription */ |
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int _params_sub; /**< notification of parameter updates */ |
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int _manual_control_sub; /**< notification of manual control updates */ |
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int _mission_sub; |
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orb_advert_t _att_pub; /**< position setpoint */ |
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struct vehicle_attitude_s _att; /**< vehicle attitude */ |
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struct vehicle_attitude_setpoint_s _att_sp; /**< vehicle attitude setpoint */ |
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struct manual_control_setpoint_s _manual; /**< r/c channel data */ |
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struct gyro_report _gyro; |
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struct accel_report _accel; |
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struct mag_report _mag; |
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struct airspeed_s _airspeed; /**< airspeed */ |
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struct vehicle_status_s _vstatus; /**< vehicle status */ |
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struct vehicle_global_position_s _global_pos; /**< global vehicle position */ |
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perf_counter_t _loop_perf; /**< loop performance counter */ |
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unsigned _mission_items_maxcount; /**< maximum number of mission items supported */ |
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struct mission_item_s * _mission_items; /**< storage for mission items */ |
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bool _mission_valid; /**< flag if mission is valid */ |
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/** manual control states */ |
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float _seatbelt_hold_heading; /**< heading the system should hold in seatbelt mode */ |
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float _loiter_hold_lat; |
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float _loiter_hold_lon; |
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float _loiter_hold_alt; |
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bool _loiter_hold; |
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struct { |
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float throttle_cruise; |
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} _parameters; /**< local copies of interesting parameters */ |
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struct { |
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param_t throttle_cruise; |
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} _parameter_handles; /**< handles for interesting parameters */ |
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/**
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* Update our local parameter cache. |
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*/ |
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int parameters_update(); |
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/**
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* Update control outputs |
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* |
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*/ |
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void control_update(); |
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/**
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* Check for changes in vehicle status. |
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*/ |
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void vehicle_status_poll(); |
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/**
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* Shim for calling task_main from task_create. |
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*/ |
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static void task_main_trampoline(int argc, char *argv[]); |
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/**
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* Main sensor collection task. |
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*/ |
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void task_main() __attribute__((noreturn)); |
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}; |
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namespace estimator |
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{ |
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/* oddly, ERROR is not defined for c++ */ |
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#ifdef ERROR |
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# undef ERROR |
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#endif |
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static const int ERROR = -1; |
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FixedwingEstimator *g_estimator; |
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} |
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FixedwingEstimator::FixedwingEstimator() : |
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_task_should_exit(false), |
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_estimator_task(-1), |
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/* subscriptions */ |
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_global_pos_sub(-1), |
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_gyro_sub(-1), |
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_accel_sub(-1), |
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_mag_sub(-1), |
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_airspeed_sub(-1), |
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_vstatus_sub(-1), |
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_params_sub(-1), |
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_manual_control_sub(-1), |
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/* publications */ |
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_att_pub(-1), |
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/* performance counters */ |
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_loop_perf(perf_alloc(PC_ELAPSED, "fw_att_pos_estimator")), |
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/* states */ |
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_mission_items_maxcount(20), |
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_mission_valid(false), |
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_loiter_hold(false) |
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{ |
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_parameter_handles.throttle_cruise = param_find("NAV_DUMMY"); |
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/* fetch initial parameter values */ |
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parameters_update(); |
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} |
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FixedwingEstimator::~FixedwingEstimator() |
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{ |
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if (_estimator_task != -1) { |
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/* task wakes up every 100ms or so at the longest */ |
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_task_should_exit = true; |
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/* wait for a second for the task to quit at our request */ |
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unsigned i = 0; |
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do { |
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/* wait 20ms */ |
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usleep(20000); |
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/* if we have given up, kill it */ |
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if (++i > 50) { |
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task_delete(_estimator_task); |
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break; |
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} |
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} while (_estimator_task != -1); |
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} |
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estimator::g_estimator = nullptr; |
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} |
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int |
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FixedwingEstimator::parameters_update() |
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{ |
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//param_get(_parameter_handles.throttle_cruise, &(_parameters.throttle_cruise));
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return OK; |
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} |
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void |
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FixedwingEstimator::vehicle_status_poll() |
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{ |
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bool vstatus_updated; |
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/* Check HIL state if vehicle status has changed */ |
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orb_check(_vstatus_sub, &vstatus_updated); |
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if (vstatus_updated) { |
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orb_copy(ORB_ID(vehicle_status), _vstatus_sub, &_vstatus); |
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} |
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} |
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void |
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FixedwingEstimator::task_main_trampoline(int argc, char *argv[]) |
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{ |
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estimator::g_estimator->task_main(); |
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} |
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void |
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FixedwingEstimator::task_main() |
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{ |
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/* inform about start */ |
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warnx("Initializing.."); |
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fflush(stdout); |
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/*
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* do subscriptions |
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*/ |
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_gyro_sub = orb_subscribe(ORB_ID(sensor_gyro)); |
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_accel_sub = orb_subscribe(ORB_ID(sensor_accel)); |
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_mag_sub = orb_subscribe(ORB_ID(sensor_mag)); |
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_airspeed_sub = orb_subscribe(ORB_ID(airspeed)); |
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_vstatus_sub = orb_subscribe(ORB_ID(vehicle_status)); |
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_params_sub = orb_subscribe(ORB_ID(parameter_update)); |
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_manual_control_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); |
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/* rate limit vehicle status updates to 5Hz */ |
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orb_set_interval(_vstatus_sub, 200); |
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/* rate limit position updates to 50 Hz */ |
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orb_set_interval(_global_pos_sub, 20); |
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parameters_update(); |
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/* wakeup source(s) */ |
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struct pollfd fds[2]; |
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/* Setup of loop */ |
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fds[0].fd = _params_sub; |
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fds[0].events = POLLIN; |
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fds[1].fd = _gyro_sub; |
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fds[1].events = POLLIN; |
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while (!_task_should_exit) { |
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/* wait for up to 500ms for data */ |
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int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 100); |
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/* timed out - periodic check for _task_should_exit, etc. */ |
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if (pret == 0) |
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continue; |
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/* this is undesirable but not much we can do - might want to flag unhappy status */ |
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if (pret < 0) { |
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warn("poll error %d, %d", pret, errno); |
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continue; |
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} |
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perf_begin(_loop_perf); |
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/* check vehicle status for changes to publication state */ |
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vehicle_status_poll(); |
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/* only update parameters if they changed */ |
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if (fds[0].revents & POLLIN) { |
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/* read from param to clear updated flag */ |
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struct parameter_update_s update; |
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orb_copy(ORB_ID(parameter_update), _params_sub, &update); |
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/* update parameters from storage */ |
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parameters_update(); |
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} |
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/* only run estimator if gyro updated */ |
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if (fds[1].revents & POLLIN) { |
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static uint64_t last_run = 0; |
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float deltaT = (hrt_absolute_time() - last_run) / 1000000.0f; |
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last_run = hrt_absolute_time(); |
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/* guard against too large deltaT's */ |
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if (deltaT > 1.0f) |
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deltaT = 0.01f; |
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/* load local copies */ |
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orb_copy(ORB_ID(sensor_gyro), _gyro_sub, &_gyro); |
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bool updated; |
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orb_check(_accel_sub, &updated); |
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if (updated) |
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orb_copy(ORB_ID(sensor_accel), _accel_sub, &_accel); |
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orb_check(_mag_sub, &updated); |
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if (updated) |
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orb_copy(ORB_ID(sensor_mag), _mag_sub, &_mag); |
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orb_check(_airspeed_sub, &updated); |
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if (updated) |
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orb_copy(ORB_ID(airspeed), _airspeed_sub, &_airspeed); |
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/* lazily publish the attitude only once available */ |
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if (_att_pub > 0) { |
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/* publish the attitude setpoint */ |
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orb_publish(ORB_ID(vehicle_attitude), _att_pub, &_att); |
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} else { |
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/* advertise and publish */ |
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_att_pub = orb_advertise(ORB_ID(vehicle_attitude), &_att); |
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} |
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} |
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perf_end(_loop_perf); |
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} |
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warnx("exiting.\n"); |
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_estimator_task = -1; |
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_exit(0); |
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} |
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int |
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FixedwingEstimator::start() |
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{ |
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ASSERT(_estimator_task == -1); |
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/* start the task */ |
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_estimator_task = task_spawn_cmd("fw_att_pos_estimator", |
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SCHED_DEFAULT, |
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SCHED_PRIORITY_MAX - 5, |
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2048, |
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(main_t)&FixedwingEstimator::task_main_trampoline, |
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nullptr); |
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if (_estimator_task < 0) { |
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warn("task start failed"); |
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return -errno; |
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} |
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return OK; |
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} |
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int fw_att_pos_estimator_main(int argc, char *argv[]) |
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{ |
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if (argc < 1) |
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errx(1, "usage: fw_att_pos_estimator {start|stop|status}"); |
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if (!strcmp(argv[1], "start")) { |
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if (estimator::g_estimator != nullptr) |
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errx(1, "already running"); |
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estimator::g_estimator = new FixedwingEstimator; |
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if (estimator::g_estimator == nullptr) |
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errx(1, "alloc failed"); |
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if (OK != estimator::g_estimator->start()) { |
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delete estimator::g_estimator; |
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estimator::g_estimator = nullptr; |
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err(1, "start failed"); |
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} |
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|
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exit(0); |
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} |
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if (!strcmp(argv[1], "stop")) { |
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if (estimator::g_estimator == nullptr) |
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errx(1, "not running"); |
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delete estimator::g_estimator; |
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estimator::g_estimator = nullptr; |
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exit(0); |
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} |
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|
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if (!strcmp(argv[1], "status")) { |
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if (estimator::g_estimator) { |
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errx(0, "running"); |
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|
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} else { |
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errx(1, "not running"); |
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} |
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} |
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warnx("unrecognized command"); |
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return 1; |
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} |
@ -0,0 +1,52 @@
@@ -0,0 +1,52 @@
|
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/****************************************************************************
|
||||
* |
||||
* 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 |
||||
* 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. |
||||
* |
||||
****************************************************************************/ |
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|
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/**
|
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* @file fw_att_pos_estimator_params.c |
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* |
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* Parameters defined by the attitude and position estimator task |
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* |
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* @author Lorenz Meier <lm@inf.ethz.ch> |
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*/ |
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|
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#include <nuttx/config.h> |
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|
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#include <systemlib/param/param.h> |
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|
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/*
|
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* Estimator parameters, accessible via MAVLink |
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* |
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*/ |
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|
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PARAM_DEFINE_FLOAT(NAV_DUMMY, 0.0f); |
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|
@ -0,0 +1,41 @@
@@ -0,0 +1,41 @@
|
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############################################################################
|
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#
|
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# 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
|
||||
# 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.
|
||||
#
|
||||
############################################################################
|
||||
|
||||
#
|
||||
# Main Attitude and Position Estimator for Fixed Wing Aircraft
|
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#
|
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|
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MODULE_COMMAND = navigator
|
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|
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SRCS = fw_att_pos_estimator_main.cpp \
|
||||
fw_att_pos_estimator_params.c
|
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Reference in new issue