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219 lines
6.1 KiB
219 lines
6.1 KiB
#pragma once |
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#include <AP_HAL/AP_HAL.h> |
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#if CONFIG_HAL_BOARD == HAL_BOARD_SITL |
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#include "AP_HAL_SITL.h" |
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#include "AP_HAL_SITL_Namespace.h" |
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#include "HAL_SITL_Class.h" |
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#include "RCInput.h" |
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#include <sys/types.h> |
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#include <sys/socket.h> |
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#include <netinet/in.h> |
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#include <netinet/udp.h> |
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#include <arpa/inet.h> |
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#include <AP_Baro/AP_Baro.h> |
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#include <AP_InertialSensor/AP_InertialSensor.h> |
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#include <AP_Compass/AP_Compass.h> |
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#include <AP_OpticalFlow/AP_OpticalFlow.h> |
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#include <AP_Terrain/AP_Terrain.h> |
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#include <SITL/SITL.h> |
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#include <SITL/SIM_Gimbal.h> |
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#include <SITL/SIM_ADSB.h> |
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#include <AP_HAL/utility/Socket.h> |
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class HAL_SITL; |
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class HALSITL::SITL_State { |
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friend class HALSITL::Scheduler; |
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friend class HALSITL::Util; |
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public: |
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void init(int argc, char * const argv[]); |
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enum vehicle_type { |
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ArduCopter, |
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APMrover2, |
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ArduPlane |
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}; |
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int gps_pipe(void); |
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int gps2_pipe(void); |
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ssize_t gps_read(int fd, void *buf, size_t count); |
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uint16_t pwm_output[SITL_NUM_CHANNELS]; |
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uint16_t last_pwm_output[SITL_NUM_CHANNELS]; |
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uint16_t pwm_input[SITL_RC_INPUT_CHANNELS]; |
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bool new_rc_input; |
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void loop_hook(void); |
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uint16_t base_port(void) const { |
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return _base_port; |
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} |
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// simulated airspeed, sonar and battery monitor |
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uint16_t sonar_pin_value; // pin 0 |
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uint16_t airspeed_pin_value; // pin 1 |
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uint16_t voltage_pin_value; // pin 13 |
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uint16_t current_pin_value; // pin 12 |
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// return TCP client address for uartC |
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const char *get_client_address(void) const { return _client_address; } |
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// paths for UART devices |
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const char *_uart_path[5] { |
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"tcp:0:wait", |
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"GPS1", |
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"tcp:2", |
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"tcp:3", |
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"GPS2" |
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}; |
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private: |
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void _parse_command_line(int argc, char * const argv[]); |
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void _set_param_default(const char *parm); |
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void _usage(void); |
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void _sitl_setup(const char *home_str); |
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void _setup_fdm(void); |
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void _setup_timer(void); |
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void _setup_adc(void); |
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float height_agl(void); |
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void _update_barometer(float height); |
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void _update_compass(float rollDeg, float pitchDeg, float yawDeg); |
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void _update_flow(void); |
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struct gps_data { |
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double latitude; |
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double longitude; |
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float altitude; |
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double speedN; |
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double speedE; |
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double speedD; |
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bool have_lock; |
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}; |
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#define MAX_GPS_DELAY 100 |
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gps_data _gps_data[MAX_GPS_DELAY]; |
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bool _gps_has_basestation_position; |
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gps_data _gps_basestation_data; |
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void _gps_write(const uint8_t *p, uint16_t size); |
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void _gps_send_ubx(uint8_t msgid, uint8_t *buf, uint16_t size); |
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void _update_gps_ubx(const struct gps_data *d); |
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void _update_gps_mtk(const struct gps_data *d); |
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void _update_gps_mtk16(const struct gps_data *d); |
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void _update_gps_mtk19(const struct gps_data *d); |
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uint16_t _gps_nmea_checksum(const char *s); |
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void _gps_nmea_printf(const char *fmt, ...); |
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void _update_gps_nmea(const struct gps_data *d); |
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void _sbp_send_message(uint16_t msg_type, uint16_t sender_id, uint8_t len, uint8_t *payload); |
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void _update_gps_sbp(const struct gps_data *d); |
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void _update_gps_file(const struct gps_data *d); |
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void _update_gps(double latitude, double longitude, float altitude, |
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double speedN, double speedE, double speedD, bool have_lock); |
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void _update_ins(float roll, float pitch, float yaw, // Relative to earth |
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double rollRate, double pitchRate,double yawRate, // Local to plane |
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double xAccel, double yAccel, double zAccel, // Local to plane |
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float airspeed, float altitude); |
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void _fdm_input(void); |
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void _fdm_input_local(void); |
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void _output_to_flightgear(void); |
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void _simulator_servos(SITL::Aircraft::sitl_input &input); |
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void _simulator_output(bool synthetic_clock_mode); |
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void _apply_servo_filter(float deltat); |
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uint16_t _airspeed_sensor(float airspeed); |
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uint16_t _ground_sonar(); |
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float _rand_float(void); |
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Vector3f _rand_vec3f(void); |
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void _fdm_input_step(void); |
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void wait_clock(uint64_t wait_time_usec); |
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// internal state |
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enum vehicle_type _vehicle; |
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uint16_t _framerate; |
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uint8_t _instance; |
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uint16_t _base_port; |
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struct sockaddr_in _rcout_addr; |
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pid_t _parent_pid; |
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uint32_t _update_count; |
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AP_Baro *_barometer; |
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AP_InertialSensor *_ins; |
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Scheduler *_scheduler; |
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Compass *_compass; |
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OpticalFlow *_optical_flow; |
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AP_Terrain *_terrain; |
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SocketAPM _sitl_rc_in{true}; |
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SITL::SITL *_sitl; |
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uint16_t _rcout_port; |
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uint16_t _simin_port; |
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float _current; |
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bool _synthetic_clock_mode; |
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const char *_fdm_address; |
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// delay buffer variables |
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static const uint8_t mag_buffer_length = 250; |
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static const uint8_t wind_buffer_length = 50; |
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static const uint8_t baro_buffer_length = 50; |
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// magnetometer delay buffer variables |
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struct readings_mag { |
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uint32_t time; |
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Vector3f data; |
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}; |
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uint8_t store_index_mag; |
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uint32_t last_store_time_mag; |
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VectorN<readings_mag,mag_buffer_length> buffer_mag; |
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uint32_t time_delta_mag; |
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uint32_t delayed_time_mag; |
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// airspeed sensor delay buffer variables |
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struct readings_wind { |
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uint32_t time; |
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float data; |
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}; |
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uint8_t store_index_wind; |
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uint32_t last_store_time_wind; |
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VectorN<readings_wind,wind_buffer_length> buffer_wind; |
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uint32_t time_delta_wind; |
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uint32_t delayed_time_wind; |
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// barometer delay buffer variables |
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struct readings_baro { |
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uint32_t time; |
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float data; |
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}; |
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uint8_t store_index_baro; |
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uint32_t last_store_time_baro; |
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VectorN<readings_baro,baro_buffer_length> buffer_baro; |
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uint32_t time_delta_baro; |
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uint32_t delayed_time_baro; |
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// internal SITL model |
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SITL::Aircraft *sitl_model; |
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// simulated gimbal |
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bool enable_gimbal; |
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SITL::Gimbal *gimbal; |
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// simulated gimbal |
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bool enable_ADSB; |
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SITL::ADSB *adsb; |
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// output socket for flightgear viewing |
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SocketAPM fg_socket{true}; |
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// TCP address to connect uartC to |
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const char *_client_address; |
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const char *defaults_path = HAL_PARAM_DEFAULTS_PATH; |
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}; |
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#endif // CONFIG_HAL_BOARD == HAL_BOARD_SITL
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