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219 lines
8.0 KiB
C++
219 lines
8.0 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2019 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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#pragma once
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#include <px4_module.h>
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#include <px4_module_params.h>
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#include <px4_posix.h>
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#include <matrix/matrix/math.hpp> // matrix, vectors, dcm, quaterions
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#include <conversion/rotation.h> // math::radians,
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#include <ecl/geo/geo.h> // to get the physical constants
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#include <drivers/drv_hrt.h> // to get the real time
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#include <perf/perf_counter.h>
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#include <uORB/topics/parameter_update.h>
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#include <uORB/topics/actuator_outputs.h>
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#include <uORB/topics/sensor_baro.h>
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#include <uORB/topics/sensor_gyro.h>
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#include <uORB/topics/sensor_accel.h>
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#include <uORB/topics/sensor_mag.h>
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#include <uORB/topics/vehicle_gps_position.h>
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#include <uORB/topics/vehicle_global_position.h> // to publish groundtruth
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#include <uORB/topics/vehicle_attitude.h> // to publish groundtruth
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using namespace matrix;
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extern "C" __EXPORT int sih_main(int argc, char *argv[]);
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class Sih : public ModuleBase<Sih>, public ModuleParams
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{
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public:
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Sih(int example_param, bool example_flag);
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virtual ~Sih() = default;
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/** @see ModuleBase */
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static int task_spawn(int argc, char *argv[]);
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/** @see ModuleBase */
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static Sih *instantiate(int argc, char *argv[]);
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/** @see ModuleBase */
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static int custom_command(int argc, char *argv[]);
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/** @see ModuleBase */
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static int print_usage(const char *reason = nullptr);
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/** @see ModuleBase::run() */
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void run() override;
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/** @see ModuleBase::print_status() */
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int print_status() override;
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static float generate_wgn(); // generate white Gaussian noise sample
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// generate white Gaussian noise sample as a 3D vector with specified std
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static Vector3f noiseGauss3f(float stdx, float stdy, float stdz);
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// timer called periodically to post the semaphore
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static void timer_callback(void *sem);
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// static int pack_float(char* uart_msg, int index, void *value); // pack a float to a IEEE754
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private:
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/**
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* Check for parameter changes and update them if needed.
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* @param parameter_update_sub uorb subscription to parameter_update
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* @param force for a parameter update
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*/
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void parameters_update_poll();
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void parameters_updated();
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// to publish the sensor baro
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struct sensor_baro_s _sensor_baro {};
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orb_advert_t _sensor_baro_pub{nullptr};
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// to publish the sensor mag
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struct sensor_mag_s _sensor_mag {};
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orb_advert_t _sensor_mag_pub{nullptr};
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// to publish the sensor gyroscope
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struct sensor_gyro_s _sensor_gyro {};
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orb_advert_t _sensor_gyro_pub{nullptr};
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// to publish the sensor accelerometer
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struct sensor_accel_s _sensor_accel {};
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orb_advert_t _sensor_accel_pub{nullptr};
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// to publish the gps position
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struct vehicle_gps_position_s _vehicle_gps_pos {};
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orb_advert_t _vehicle_gps_pos_pub{nullptr};
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// attitude groundtruth
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struct vehicle_global_position_s _gpos_gt {};
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orb_advert_t _gpos_gt_sub{nullptr};
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// global position groundtruth
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struct vehicle_attitude_s _att_gt {};
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orb_advert_t _att_gt_sub{nullptr};
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int _parameter_update_sub {-1};
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int _actuator_out_sub {-1};
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// hard constants
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static constexpr uint16_t NB_MOTORS = 4;
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static constexpr float T1_C = 15.0f; // ground temperature in celcius
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static constexpr float T1_K = T1_C - CONSTANTS_ABSOLUTE_NULL_CELSIUS; // ground temperature in Kelvin
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static constexpr float TEMP_GRADIENT = -6.5f / 1000.0f; // temperature gradient in degrees per metre
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static constexpr hrt_abstime LOOP_INTERVAL = 4000; // 4ms => 250 Hz real-time
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void init_variables();
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void init_sensors();
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void read_motors();
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void generate_force_and_torques();
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void equations_of_motion();
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void reconstruct_sensors_signals();
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void send_IMU();
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void send_gps();
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void publish_sih();
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void inner_loop();
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perf_counter_t _loop_perf;
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perf_counter_t _sampling_perf;
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px4_sem_t _data_semaphore;
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int32_t _counter = 0;
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hrt_call _timer_call;
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hrt_abstime _last_run;
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hrt_abstime _gps_time;
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hrt_abstime _serial_time;
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hrt_abstime _now;
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float _dt; // sampling time [s]
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Vector3f _T_B; // thrust force in body frame [N]
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Vector3f _Fa_I; // aerodynamic force in inertial frame [N]
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Vector3f _Mt_B; // thruster moments in the body frame [Nm]
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Vector3f _Ma_B; // aerodynamic moments in the body frame [Nm]
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Vector3f _p_I; // inertial position [m]
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Vector3f _v_I; // inertial velocity [m/s]
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Vector3f _v_B; // body frame velocity [m/s]
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Vector3f _p_I_dot; // inertial position differential
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Vector3f _v_I_dot; // inertial velocity differential
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Quatf _q; // quaternion attitude
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Dcmf _C_IB; // body to inertial transformation
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Vector3f _w_B; // body rates in body frame [rad/s]
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Quatf _q_dot; // quaternion differential
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Vector3f _w_B_dot; // body rates differential
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float _u[NB_MOTORS]; // thruster signals
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// sensors reconstruction
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Vector3f _acc;
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Vector3f _mag;
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Vector3f _gyro;
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Vector3f _gps_vel;
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double _gps_lat, _gps_lat_noiseless;
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double _gps_lon, _gps_lon_noiseless;
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float _gps_alt, _gps_alt_noiseless;
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float _baro_p_mBar; // reconstructed (simulated) pressure in mBar
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float _baro_temp_c; // reconstructed (simulated) barometer temperature in celcius
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// parameters
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float _MASS, _T_MAX, _Q_MAX, _L_ROLL, _L_PITCH, _KDV, _KDW, _H0;
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double _LAT0, _LON0, _COS_LAT0;
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Vector3f _W_I; // weight of the vehicle in inertial frame [N]
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Matrix3f _I; // vehicle inertia matrix
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Matrix3f _Im1; // inverse of the intertia matrix
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Vector3f _mu_I; // NED magnetic field in inertial frame [G]
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// parameters defined in sih_params.c
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DEFINE_PARAMETERS(
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(ParamFloat<px4::params::SIH_MASS>) _sih_mass,
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(ParamFloat<px4::params::SIH_IXX>) _sih_ixx,
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(ParamFloat<px4::params::SIH_IYY>) _sih_iyy,
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(ParamFloat<px4::params::SIH_IZZ>) _sih_izz,
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(ParamFloat<px4::params::SIH_IXY>) _sih_ixy,
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(ParamFloat<px4::params::SIH_IXZ>) _sih_ixz,
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(ParamFloat<px4::params::SIH_IYZ>) _sih_iyz,
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(ParamFloat<px4::params::SIH_T_MAX>) _sih_t_max,
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(ParamFloat<px4::params::SIH_Q_MAX>) _sih_q_max,
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(ParamFloat<px4::params::SIH_L_ROLL>) _sih_l_roll,
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(ParamFloat<px4::params::SIH_L_PITCH>) _sih_l_pitch,
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(ParamFloat<px4::params::SIH_KDV>) _sih_kdv,
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(ParamFloat<px4::params::SIH_KDW>) _sih_kdw,
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(ParamInt<px4::params::SIH__LAT0>) _sih_lat0,
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(ParamInt<px4::params::SIH__LON0>) _sih_lon0,
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(ParamFloat<px4::params::SIH__H0>) _sih_h0,
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(ParamFloat<px4::params::SIH__MU_X>) _sih_mu_x,
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(ParamFloat<px4::params::SIH__MU_Y>) _sih_mu_y,
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(ParamFloat<px4::params::SIH__MU_Z>) _sih_mu_z
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)
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};
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