mirror of https://github.com/ArduPilot/ardupilot
132 lines
3.9 KiB
C++
132 lines
3.9 KiB
C++
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#ifndef __AP_HAL_AVR_SITL_STATE_H__
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#define __AP_HAL_AVR_SITL_STATE_H__
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#include <AP_HAL.h>
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#if CONFIG_HAL_BOARD == HAL_BOARD_AVR_SITL
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#include <AP_HAL_AVR_SITL.h>
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#include "AP_HAL_AVR_SITL_Namespace.h"
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#include "HAL_AVR_SITL_Class.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 "../SITL/SITL.h"
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class HAL_AVR_SITL;
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class AVR_SITL::SITL_State {
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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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static uint16_t pwm_output[11];
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static uint16_t last_pwm_output[11];
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static uint16_t pwm_input[8];
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static bool new_rc_input;
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static void loop_hook(void);
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uint16_t base_port(void) const { return _base_port; }
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// simulated airspeed, sonar and battery monitor
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static uint16_t sonar_pin_value; // pin 0
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static uint16_t airspeed_pin_value; // pin 1
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static uint16_t voltage_pin_value; // pin 13
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static uint16_t current_pin_value; // pin 12
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private:
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void _parse_command_line(int argc, char * const argv[]);
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void _usage(void);
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void _sitl_setup(void);
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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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// these methods are static as they are called
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// from the timer
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static void _update_barometer(float height);
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static void _update_compass(float rollDeg, float pitchDeg, float yawDeg);
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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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static gps_data _gps_data[MAX_GPS_DELAY];
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static void _gps_write(const uint8_t *p, uint16_t size);
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static void _gps_send_ubx(uint8_t msgid, uint8_t *buf, uint16_t size);
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static void _update_gps_ubx(const struct gps_data *d);
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static void _update_gps_mtk(const struct gps_data *d);
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static void _update_gps_mtk16(const struct gps_data *d);
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static void _update_gps_mtk19(const struct gps_data *d);
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static uint16_t _gps_nmea_checksum(const char *s);
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static void _gps_nmea_printf(const char *fmt, ...);
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static void _update_gps_nmea(const struct gps_data *d);
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static 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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static 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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static void _fdm_input(void);
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static void _simulator_output(void);
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static void _apply_servo_filter(float deltat);
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static uint16_t _airspeed_sensor(float airspeed);
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static uint16_t _ground_sonar(float altitude);
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static float _gyro_drift(void);
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static float _rand_float(void);
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static Vector3f _rand_vec3f(void);
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// signal handlers
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static void _sig_fpe(int signum);
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static void _timer_handler(int signum);
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// internal state
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static enum vehicle_type _vehicle;
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static uint16_t _framerate;
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static uint16_t _base_port;
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float _initial_height;
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static struct sockaddr_in _rcout_addr;
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static pid_t _parent_pid;
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static uint32_t _update_count;
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static bool _motors_on;
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static AP_Baro_HIL *_barometer;
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static AP_InertialSensor_HIL *_ins;
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static SITLScheduler *_scheduler;
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static AP_Compass_HIL *_compass;
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static int _sitl_fd;
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static SITL *_sitl;
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static uint16_t _rcout_port;
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static uint16_t _simin_port;
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};
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#endif // CONFIG_HAL_BOARD == HAL_BOARD_AVR_SITL
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#endif // __AP_HAL_AVR_SITL_STATE_H__
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