ardupilot/libraries/AP_HAL_SITL/SITL_State.cpp

#include <AP_HAL/AP_HAL.h>

#if CONFIG_HAL_BOARD == HAL_BOARD_SITL && !defined(HAL_BUILD_AP_PERIPH)

#include "AP_HAL_SITL.h"
#include "AP_HAL_SITL_Namespace.h"
#include "HAL_SITL_Class.h"
#include "UARTDriver.h"
#include "Scheduler.h"
#include "CANSocketIface.h"

#include <stdio.h>
#include <signal.h>
#include <unistd.h>
#include <stdlib.h>
#include <errno.h>
#include <sys/select.h>

#include <AP_Param/AP_Param.h>
#include <SITL/SIM_JSBSim.h>
#include <AP_HAL/utility/Socket.h>

extern const AP_HAL::HAL& hal;

using namespace HALSITL;

void SITL_State::_set_param_default(const char *parm)
{
    char *pdup = strdup(parm);
    char *p = strchr(pdup, '=');
    if (p == nullptr) {
        printf("Please specify parameter as NAME=VALUE");
        exit(1);
    }
    float value = strtof(p+1, nullptr);
    *p = 0;
    enum ap_var_type var_type;
    AP_Param *vp = AP_Param::find(pdup, &var_type);
    if (vp == nullptr) {
        printf("Unknown parameter %s\n", pdup);
        exit(1);
    }
    if (var_type == AP_PARAM_FLOAT) {
        ((AP_Float *)vp)->set_and_save(value);
    } else if (var_type == AP_PARAM_INT32) {
        ((AP_Int32 *)vp)->set_and_save(value);
    } else if (var_type == AP_PARAM_INT16) {
        ((AP_Int16 *)vp)->set_and_save(value);
    } else if (var_type == AP_PARAM_INT8) {
        ((AP_Int8 *)vp)->set_and_save(value);
    } else {
        printf("Unable to set parameter %s\n", pdup);
        exit(1);
    }
    printf("Set parameter %s to %f\n", pdup, value);
    free(pdup);
}


/*
  setup for SITL handling
 */
void SITL_State::_sitl_setup()
{
#if !defined(__CYGWIN__) && !defined(__CYGWIN64__)
    _parent_pid = getppid();
#endif

    _setup_fdm();
    fprintf(stdout, "Starting SITL input\n");

    // find the barometer object if it exists
    _sitl = AP::sitl();

    if (_sitl != nullptr) {
        // setup some initial values
        _update_airspeed(0);
        if (enable_gimbal) {
            gimbal = new SITL::Gimbal(_sitl->state);
        }

        sitl_model->set_buzzer(&_sitl->buzzer_sim);
        sitl_model->set_sprayer(&_sitl->sprayer_sim);
        sitl_model->set_gripper_servo(&_sitl->gripper_sim);
        sitl_model->set_gripper_epm(&_sitl->gripper_epm_sim);
        sitl_model->set_parachute(&_sitl->parachute_sim);
        sitl_model->set_precland(&_sitl->precland_sim);
        _sitl->i2c_sim.init();
        sitl_model->set_i2c(&_sitl->i2c_sim);
#if AP_TEST_DRONECAN_DRIVERS
        sitl_model->set_dronecan_device(&_sitl->dronecan_sim);
#endif
        if (_use_fg_view) {
            fg_socket.connect(_fg_address, _fg_view_port);
        }

        fprintf(stdout, "Using Irlock at port : %d\n", _irlock_port);
        _sitl->irlock_port = _irlock_port;
    }

    if (_synthetic_clock_mode) {
        // start with non-zero clock
        hal.scheduler->stop_clock(1);
    }
}


/*
  setup a SITL FDM listening UDP port
 */
void SITL_State::_setup_fdm(void)
{
    if (!_sitl_rc_in.reuseaddress()) {
        fprintf(stderr, "SITL: socket reuseaddress failed on RC in port: %d - %s\n", _rcin_port, strerror(errno));
        fprintf(stderr, "Aborting launch...\n");
        exit(1);
    }
    if (!_sitl_rc_in.bind("0.0.0.0", _rcin_port)) {
        fprintf(stderr, "SITL: socket bind failed on RC in port : %d - %s\n", _rcin_port, strerror(errno));
        fprintf(stderr, "Aborting launch...\n");
        exit(1);
    }
    if (!_sitl_rc_in.set_blocking(false)) {
        fprintf(stderr, "SITL: socket set_blocking(false) failed on RC in port: %d - %s\n", _rcin_port, strerror(errno));
        fprintf(stderr, "Aborting launch...\n");
        exit(1);
    }
    if (!_sitl_rc_in.set_cloexec()) {
        fprintf(stderr, "SITL: socket set_cloexec() failed on RC in port: %d - %s\n", _rcin_port, strerror(errno));
        fprintf(stderr, "Aborting launch...\n");
        exit(1);
    }
}


/*
  step the FDM by one time step
 */
void SITL_State::_fdm_input_step(void)
{
    static uint32_t last_pwm_input = 0;

    _fdm_input_local();

    /* make sure we die if our parent dies */
    if (kill(_parent_pid, 0) != 0) {
        exit(1);
    }

    if (_scheduler->interrupts_are_blocked() || _sitl == nullptr) {
        return;
    }

    // simulate RC input at 50Hz
    if (AP_HAL::millis() - last_pwm_input >= 20 && _sitl != nullptr && _sitl->rc_fail != SITL::SIM::SITL_RCFail_NoPulses) {
        last_pwm_input = AP_HAL::millis();
        new_rc_input = true;
    }

    _scheduler->sitl_begin_atomic();

    if (_update_count == 0 && _sitl != nullptr) {
        HALSITL::Scheduler::timer_event();
        _scheduler->sitl_end_atomic();
        return;
    }

    if (_sitl != nullptr) {
        _update_airspeed(_sitl->state.airspeed);
        _update_rangefinder();
    }

    // trigger all APM timers.
    HALSITL::Scheduler::timer_event();
    _scheduler->sitl_end_atomic();
}


void SITL_State::wait_clock(uint64_t wait_time_usec)
{
    float speedup = sitl_model->get_speedup();
    if (speedup < 1) {
        // for purposes of sleeps treat low speedups as 1
        speedup = 1.0;
    }
    while (AP_HAL::micros64() < wait_time_usec) {
        if (hal.scheduler->in_main_thread() ||
            Scheduler::from(hal.scheduler)->semaphore_wait_hack_required()) {
            _fdm_input_step();
        } else {
#ifdef CYGWIN_BUILD
            if (speedup > 2 && hal.util->get_soft_armed()) {
                const char *current_thread = Scheduler::from(hal.scheduler)->get_current_thread_name();
                if (current_thread && strcmp(current_thread, "Scripting") == 0) {
                    // this effectively does a yield of the CPU. The
                    // granularity of sleeps on cygwin is very high,
                    // so this is needed for good thread performance
                    // in scripting. We don't do this at low speedups
                    // as it causes the cpu to run hot
                    // We also don't do it while disarmed, as lua performance is less
                    // critical while disarmed
                    usleep(0);
                    continue;
                }
            }
#endif
            usleep(1000);
        }
    }
    // check the outbound TCP queue size.  If it is too long then
    // MAVProxy/pymavlink take too long to process packets and it ends
    // up seeing traffic well into our past and hits time-out
    // conditions.
    if (speedup > 1 && hal.scheduler->in_main_thread()) {
        while (true) {
            const int queue_length = ((HALSITL::UARTDriver*)hal.serial(0))->get_system_outqueue_length();
            // ::fprintf(stderr, "queue_length=%d\n", (signed)queue_length);
            if (queue_length < 1024) {
                break;
            }
            usleep(1000);
        }
    }
}

/*
  check for a SITL RC input packet
 */
void SITL_State::_check_rc_input(void)
{
    uint32_t count = 0;
    while (_read_rc_sitl_input()) {
        count++;
    }

    if (count > 100) {
        ::fprintf(stderr, "Read %u rc inputs\n", count);
    }
}

bool SITL_State::_read_rc_sitl_input()
{
    struct pwm_packet {
        uint16_t pwm[16];
    } pwm_pkt;

    const ssize_t size = _sitl_rc_in.recv(&pwm_pkt, sizeof(pwm_pkt), 0);

    // if we are simulating no pulses RC failure, do not update pwm_input
    if (_sitl->rc_fail == SITL::SIM::SITL_RCFail_NoPulses) {
        return size != -1; // we must continue to drain _sitl_rc
    }

    if (_sitl->rc_fail == SITL::SIM::SITL_RCFail_Throttle950) {
        // discard anything we just read from the "receiver" and set
        // values to bind values:
        for (uint8_t i=0; i<ARRAY_SIZE(pwm_input); i++) {
            pwm_input[0] = 1500;  // centre all inputs
        }
        pwm_input[2] = 950;  // reset throttle (assumed to be on channel 3...)
        return size != -1;  // we must continue to drain _sitl_rc
    }

    switch (size) {
    case -1:
        return false;
    case 8*2:
    case 16*2: {
        // a packet giving the receiver PWM inputs
        for (uint8_t i=0; i<size/2; i++) {
            // setup the pwm input for the RC channel inputs
            if (i < _sitl->state.rcin_chan_count) {
                // we're using rc from simulator
                continue;
            }
            uint16_t pwm = pwm_pkt.pwm[i];
            if (pwm != 0) {
                pwm_input[i] = pwm;
            }
        }
        return true;
    }
    default:
        fprintf(stderr, "Malformed SITL RC input (%ld)", (long)size);
    }
    return false;
}

/*
  output current state to flightgear
 */
void SITL_State::_output_to_flightgear(void)
{
    SITL::FGNetFDM fdm {};
    const SITL::sitl_fdm &sfdm = _sitl->state;

    fdm.version = 0x18;
    fdm.padding = 0;
    fdm.longitude = DEG_TO_RAD_DOUBLE*sfdm.longitude;
    fdm.latitude = DEG_TO_RAD_DOUBLE*sfdm.latitude;
    fdm.altitude = sfdm.altitude;
    fdm.agl = sfdm.altitude;
    fdm.phi   = radians(sfdm.rollDeg);
    fdm.theta = radians(sfdm.pitchDeg);
    fdm.psi   = radians(sfdm.yawDeg);
    fdm.vcas  = sfdm.velocity_air_bf.length()/0.3048;
    if (_vehicle == ArduCopter) {
        fdm.num_engines = 4;
        for (uint8_t i=0; i<4; i++) {
            fdm.rpm[i] = constrain_float((pwm_output[i]-1000), 0, 1000);
        }
    } else {
        fdm.num_engines = 4;
        fdm.rpm[0] = constrain_float((pwm_output[2]-1000)*3, 0, 3000);
        // for quadplane
        fdm.rpm[1] = constrain_float((pwm_output[5]-1000)*12, 0, 12000);
        fdm.rpm[2] = constrain_float((pwm_output[6]-1000)*12, 0, 12000);
        fdm.rpm[3] = constrain_float((pwm_output[7]-1000)*12, 0, 12000);
    }
    fdm.ByteSwap();

    fg_socket.send(&fdm, sizeof(fdm));
}

/*
  get FDM input from a local model
 */
void SITL_State::_fdm_input_local(void)
{
    struct sitl_input input;

    // check for direct RC input
    if (_sitl != nullptr) {
        _check_rc_input();
    }

    // construct servos structure for FDM
    _simulator_servos(input);

#if HAL_SIM_JSON_MASTER_ENABLED
    // read servo inputs from ride along flight controllers
    ride_along.receive(input);
#endif

    // update the model
    sitl_model->update_model(input);

    // get FDM output from the model
    if (_sitl) {
        sitl_model->fill_fdm(_sitl->state);

#if HAL_NUM_CAN_IFACES
        if (CANIface::num_interfaces() > 0) {
            multicast_state_send();
        }
#endif

        if (_sitl->rc_fail == SITL::SIM::SITL_RCFail_None) {
            for (uint8_t i=0; i< _sitl->state.rcin_chan_count; i++) {
                pwm_input[i] = 1000 + _sitl->state.rcin[i]*1000;
            }
        }
    }

#if HAL_SIM_JSON_MASTER_ENABLED
    // output JSON state to ride along flight controllers
    ride_along.send(_sitl->state,sitl_model->get_position_relhome());
#endif

    sim_update();

    if (_sitl && _use_fg_view) {
        _output_to_flightgear();
    }

    // update simulation time
    if (_sitl) {
        hal.scheduler->stop_clock(_sitl->state.timestamp_us);
    } else {
        hal.scheduler->stop_clock(AP_HAL::micros64()+100);
    }

    set_height_agl();

    _synthetic_clock_mode = true;
    _update_count++;
}

/*
  create sitl_input structure for sending to FDM
 */
void SITL_State::_simulator_servos(struct sitl_input &input)
{
    static uint32_t last_update_usec;

    /* this maps the registers used for PWM outputs. The RC
     * driver updates these whenever it wants the channel output
     * to change */

    if (last_update_usec == 0 || !output_ready) {
        for (uint8_t i=0; i<SITL_NUM_CHANNELS; i++) {
            pwm_output[i] = 1000;
        }
        if (_vehicle == ArduPlane) {
            pwm_output[0] = pwm_output[1] = pwm_output[3] = 1500;
        }
        if (_vehicle == Rover) {
            pwm_output[0] = pwm_output[1] = pwm_output[2] = pwm_output[3] = 1500;
        }
        if (_vehicle == ArduSub) {
            pwm_output[0] = pwm_output[1] = pwm_output[2] = pwm_output[3] =
                    pwm_output[4] = pwm_output[5] = pwm_output[6] = pwm_output[7] = 1500;
        }
    }

    // output at chosen framerate
    uint32_t now = AP_HAL::micros();
    last_update_usec = now;

    float altitude = AP::baro().get_altitude();
    float wind_speed = 0;
    float wind_direction = 0;
    float wind_dir_z = 0;

    // give 5 seconds to calibrate airspeed sensor at 0 wind speed
    if (wind_start_delay_micros == 0) {
        wind_start_delay_micros = now;
    } else if (_sitl && (now - wind_start_delay_micros) > 5000000 ) {
        // The EKF does not like step inputs so this LPF keeps it happy.
        wind_speed =     _sitl->wind_speed_active     = (0.95f*_sitl->wind_speed_active)     + (0.05f*_sitl->wind_speed);
        wind_direction = _sitl->wind_direction_active = (0.95f*_sitl->wind_direction_active) + (0.05f*_sitl->wind_direction);
        wind_dir_z =     _sitl->wind_dir_z_active     = (0.95f*_sitl->wind_dir_z_active)     + (0.05f*_sitl->wind_dir_z);
        
        // pass wind into simulators using different wind types via param SIM_WIND_T*.
        switch (_sitl->wind_type) {
        case SITL::SIM::WIND_TYPE_SQRT:
            if (altitude < _sitl->wind_type_alt) {
                wind_speed *= sqrtf(MAX(altitude / _sitl->wind_type_alt, 0));
            }
            break;

        case SITL::SIM::WIND_TYPE_COEF:
            wind_speed += (altitude - _sitl->wind_type_alt) * _sitl->wind_type_coef;
            break;

        case SITL::SIM::WIND_TYPE_NO_LIMIT:
        default:
            break;
        }

        // never allow negative wind velocity
        wind_speed = MAX(wind_speed, 0);
    }

    input.wind.speed = wind_speed;
    input.wind.direction = wind_direction;
    input.wind.turbulence = _sitl?_sitl->wind_turbulance:0;
    input.wind.dir_z = wind_dir_z;

    for (uint8_t i=0; i<SITL_NUM_CHANNELS; i++) {
        if (pwm_output[i] == 0xFFFF) {
            input.servos[i] = 0;
        } else {
            input.servos[i] = pwm_output[i];
        }
    }

    if (_sitl != nullptr) {
        // FETtec ESC simulation support.  Input signals of 1000-2000
        // are positive thrust, 0 to 1000 are negative thrust.  Deeper
        // changes required to support negative thrust - potentially
        // adding a field to input.
        if (_sitl != nullptr) {
            if (_sitl->fetteconewireesc_sim.enabled()) {
                _sitl->fetteconewireesc_sim.update_sitl_input_pwm(input);
                for (uint8_t i=0; i<ARRAY_SIZE(input.servos); i++) {
                    if (input.servos[i] != 0 && input.servos[i] < 1000) {
                        AP_HAL::panic("Bad input servo value (%u)", input.servos[i]);
                    }
                }
            }
        }
    }

    float engine_mul = _sitl?_sitl->engine_mul.get():1;
    uint8_t engine_fail = _sitl?_sitl->engine_fail.get():0;
    float throttle = 0.0f;
    
    if (engine_fail >= ARRAY_SIZE(input.servos)) {
        engine_fail = 0;
    }
    // apply engine multiplier to motor defined by the SIM_ENGINE_FAIL parameter
    if (_vehicle != Rover) {
        input.servos[engine_fail] = ((input.servos[engine_fail]-1000) * engine_mul) + 1000;
    } else {
        input.servos[engine_fail] = static_cast<uint16_t>(((input.servos[engine_fail] - 1500) * engine_mul) + 1500);
    }

    if (_vehicle == ArduPlane) {
        float forward_throttle = constrain_float((input.servos[2] - 1000) / 1000.0f, 0.0f, 1.0f);
        // do a little quadplane dance
        float hover_throttle = 0.0f;
        uint8_t running_motors = 0;
        uint32_t mask = _sitl->state.motor_mask;
        uint8_t bit;
        while ((bit = __builtin_ffs(mask)) != 0) {
            uint8_t motor = bit-1;
            mask &= ~(1U<<motor);
            float motor_throttle = constrain_float((input.servos[motor] - 1000) / 1000.0f, 0.0f, 1.0f);
            // update motor_on flag
            if (!is_zero(motor_throttle)) {
                hover_throttle += motor_throttle;
                running_motors++;
            }
        }
        if (running_motors > 0) {
            hover_throttle /= running_motors;
        }
        if (!is_zero(forward_throttle)) {
            throttle = forward_throttle;
        } else {
            throttle = hover_throttle;
        }
    } else if (_vehicle == Rover) {
        input.servos[2] = static_cast<uint16_t>(constrain_int16(input.servos[2], 1000, 2000));
        input.servos[0] = static_cast<uint16_t>(constrain_int16(input.servos[0], 1000, 2000));
        throttle = fabsf((input.servos[2] - 1500) / 500.0f);
    } else {
        // run checks on each motor
        uint8_t running_motors = 0;
        uint32_t mask = _sitl->state.motor_mask;
        uint8_t bit;
        while ((bit = __builtin_ffs(mask)) != 0) {
            const uint8_t motor = bit-1;
            mask &= ~(1U<<motor);
            float motor_throttle = constrain_float((input.servos[motor] - 1000) / 1000.0f, 0.0f, 1.0f);
            // update motor_on flag
            if (!is_zero(motor_throttle)) {
                throttle += motor_throttle;
                running_motors++;
            }
        }
        if (running_motors > 0) {
            throttle /= running_motors;
        }
    }
    if (_sitl) {
        _sitl->throttle = throttle;
    }

    update_voltage_current(input, throttle);
}

void SITL_State::init(int argc, char * const argv[])
{
    pwm_input[0] = pwm_input[1] = pwm_input[3] = 1500;
    pwm_input[4] = pwm_input[7] = 1800;
    pwm_input[2] = pwm_input[5] = pwm_input[6] = 1000;

    _scheduler = Scheduler::from(hal.scheduler);
    _parse_command_line(argc, argv);
}

/*
  set height above the ground in meters
 */
void SITL_State::set_height_agl(void)
{
    static float home_alt = -1;

    if (!_sitl) {
        // in example program
        return;
    }

    if (is_equal(home_alt, -1.0f) && _sitl->state.altitude > 0) {
        // remember home altitude as first non-zero altitude
        home_alt = _sitl->state.altitude;
    }

#if AP_TERRAIN_AVAILABLE
    if (_sitl != nullptr &&
        _sitl->terrain_enable) {
        // get height above terrain from AP_Terrain. This assumes
        // AP_Terrain is working
        float terrain_height_amsl;
        Location location;
        location.lat = _sitl->state.latitude*1.0e7;
        location.lng = _sitl->state.longitude*1.0e7;

        AP_Terrain *_terrain = AP_Terrain::get_singleton();
        if (_terrain != nullptr &&
            _terrain->height_amsl(location, terrain_height_amsl, false)) {
            _sitl->height_agl = _sitl->state.altitude - terrain_height_amsl;
            return;
        }
    }
#endif

    if (_sitl != nullptr) {
        // fall back to flat earth model
        _sitl->height_agl = _sitl->state.altitude - home_alt;
    }
}

/*
  open multicast UDP
 */
void SITL_State::multicast_state_open(void)
{
    struct sockaddr_in sockaddr {};
    int ret;

#ifdef HAVE_SOCK_SIN_LEN
    sockaddr.sin_len = sizeof(sockaddr);
#endif
    sockaddr.sin_port = htons(SITL_MCAST_PORT);
    sockaddr.sin_family = AF_INET;
    sockaddr.sin_addr.s_addr = inet_addr(SITL_MCAST_IP);

    mc_out_fd = socket(AF_INET, SOCK_DGRAM, 0);
    if (mc_out_fd == -1) {
        fprintf(stderr, "socket failed - %s\n", strerror(errno));
        exit(1);
    }
    ret = fcntl(mc_out_fd, F_SETFD, FD_CLOEXEC);
    if (ret == -1) {
        fprintf(stderr, "fcntl failed on setting FD_CLOEXEC - %s\n", strerror(errno));
        exit(1);
    }

    // try to setup for broadcast, this may fail if insufficient privileges
    int one = 1;
    setsockopt(mc_out_fd,SOL_SOCKET,SO_BROADCAST,(char *)&one,sizeof(one));

    ret = connect(mc_out_fd, (struct sockaddr *)&sockaddr, sizeof(sockaddr));
    if (ret == -1) {
        fprintf(stderr, "udp connect failed on port %u - %s\n",
                (unsigned)ntohs(sockaddr.sin_port),
                strerror(errno));
        exit(1);
    }
}

/*
  send out SITL state as multicast UDP
 */
void SITL_State::multicast_state_send(void)
{
    if (_sitl == nullptr) {
        return;
    }
    if (mc_out_fd == -1) {
        multicast_state_open();
    }
    const auto &sfdm = _sitl->state;
    send(mc_out_fd, (void*)&sfdm, sizeof(sfdm), 0);
}

#endif