ardupilot/libraries/SITL/SIM_FlightAxis.cpp

/*
   This program is free software: you can redistribute it and/or modify
   it under the terms of the GNU General Public License as published by
   the Free Software Foundation, either version 3 of the License, or
   (at your option) any later version.

   This program is distributed in the hope that it will be useful,
   but WITHOUT ANY WARRANTY; without even the implied warranty of
   MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
   GNU General Public License for more details.

   You should have received a copy of the GNU General Public License
   along with this program.  If not, see <http://www.gnu.org/licenses/>.
 */
/*
  simulator connector for FlightAxis
*/

#include "SIM_FlightAxis.h"

#include <arpa/inet.h>
#include <errno.h>
#include <fcntl.h>
#include <stdio.h>
#include <stdarg.h>
#include <sys/stat.h>
#include <sys/types.h>

#include <AP_HAL/AP_HAL.h>
#include <DataFlash/DataFlash.h>

extern const AP_HAL::HAL& hal;

namespace SITL {

// the asprintf() calls are not worth checking for SITL
#pragma GCC diagnostic ignored "-Wunused-result"

FlightAxis::FlightAxis(const char *home_str, const char *frame_str) :
    Aircraft(home_str, frame_str)
{
    use_time_sync = false;
    rate_hz = 250 / target_speedup;
    heli_demix = strstr(frame_str, "helidemix") != nullptr;
    rev4_servos = strstr(frame_str, "rev4") != nullptr;
    const char *colon = strchr(frame_str, ':');
    if (colon) {
        controller_ip = colon+1;
    }
    // FlightAxis sensor data is not good enough for EKF. Use fake EKF by default
    AP_Param::set_default_by_name("AHRS_EKF_TYPE", 10);
    AP_Param::set_default_by_name("INS_GYR_CAL", 0);

    if (strstr(frame_str, "pitch270")) {
        // rotate tailsitter airframes for fixed wing view
        rotation = ROTATION_PITCH_270;
    }
    if (strstr(frame_str, "pitch90")) {
        // rotate tailsitter airframes for fixed wing view
        rotation = ROTATION_PITCH_90;
    }

    switch (rotation) {
    case ROTATION_NONE:
        break;
    case ROTATION_PITCH_90:
        att_rotation.from_euler(0, radians(90), 0);
        break;
    case ROTATION_PITCH_270:
        att_rotation.from_euler(0, radians(270), 0);
        break;
    default:
        AP_HAL::panic("Unsupported flightaxis rotation %u\n", (unsigned)rotation);
    }
}

/*
  extremely primitive SOAP parser that assumes the format used by FlightAxis
*/
void FlightAxis::parse_reply(const char *reply)
{
    const char *reply0 = reply;
    for (uint16_t i=0; i<num_keys; i++) {
        const char *p = strstr(reply, keytable[i].key);
        if (p == nullptr) {
            p = strstr(reply0, keytable[i].key);
        }
        if (p == nullptr) {
            printf("Failed to find key %s\n", keytable[i].key);
            controller_started = false;
            break;
        }
        p += strlen(keytable[i].key) + 1;
        double v;
        if (strncmp(p, "true", 4) == 0) {
            v = 1;
        } else if (strncmp(p, "false", 5) == 0) {
            v = 0;
        } else {
            v = atof(p);
        }
        keytable[i].ref = v;
        // this assumes key order and allows us to decode arrays
        p = strchr(p, '>');
        if (p != nullptr) {
            reply = p;
        }
    }
}


/*
  make a SOAP request, returning body of reply
 */
char *FlightAxis::soap_request(const char *action, const char *fmt, ...)
{
    va_list ap;
    char *req1;

    va_start(ap, fmt);
    vasprintf(&req1, fmt, ap);
    va_end(ap);

    //printf("%s\n", req1);

    // open SOAP socket to FlightAxis
    SocketAPM sock(false);
    if (!sock.connect(controller_ip, controller_port)) {
        free(req1);
        return nullptr;
    }
    sock.set_blocking(false);

    char *req;
    asprintf(&req, R"(POST / HTTP/1.1
soapaction: '%s'
content-length: %u
content-type: text/xml;charset='UTF-8'
Connection: Keep-Alive

%s)",
             action,
             (unsigned)strlen(req1), req1);
    sock.send(req, strlen(req));
    free(req1);
    free(req);
    char reply[10000];
    memset(reply, 0, sizeof(reply));
    ssize_t ret = sock.recv(reply, sizeof(reply)-1, 1000);
    if (ret <= 0) {
        printf("No data\n");
        return nullptr;
    }
    char *p = strstr(reply, "Content-Length: ");
    if (p == nullptr) {
        printf("No Content-Length\n");
        return nullptr;
    }

    // get the content length
    uint32_t content_length = strtoul(p+16, nullptr, 10);
    char *body = strstr(p, "\r\n\r\n");
    if (body == nullptr) {
        printf("No body\n");
        return nullptr;
    }
    body += 4;

    // get the rest of the body
    int32_t expected_length = content_length + (body - reply);
    if (expected_length >= (int32_t)sizeof(reply)) {
        printf("Reply too large %i\n", expected_length);
        return nullptr;
    }
    while (ret < expected_length) {
        ssize_t ret2 = sock.recv(&reply[ret], sizeof(reply)-(1+ret), 100);
        if (ret2 <= 0) {
            return nullptr;
        }
        // nul terminate
        reply[ret+ret2] = 0;
        ret += ret2;
    }
    return strdup(reply);
}



void FlightAxis::exchange_data(const struct sitl_input &input)
{
    if (!controller_started ||
        is_zero(state.m_flightAxisControllerIsActive) ||
        !is_zero(state.m_resetButtonHasBeenPressed)) {
        printf("Starting controller at %s\n", controller_ip);
        // call a restore first. This allows us to connect after the aircraft is changed in RealFlight
        char *reply = soap_request("RestoreOriginalControllerDevice", R"(<?xml version='1.0' encoding='UTF-8'?>
<soap:Envelope xmlns:soap='http://schemas.xmlsoap.org/soap/envelope/' xmlns:xsd='http://www.w3.org/2001/XMLSchema' xmlns:xsi='http://www.w3.org/2001/XMLSchema-instance'>
<soap:Body>
<RestoreOriginalControllerDevice><a>1</a><b>2</b></RestoreOriginalControllerDevice>
</soap:Body>
</soap:Envelope>)");
        free(reply);
        reply = soap_request("InjectUAVControllerInterface", R"(<?xml version='1.0' encoding='UTF-8'?>
<soap:Envelope xmlns:soap='http://schemas.xmlsoap.org/soap/envelope/' xmlns:xsd='http://www.w3.org/2001/XMLSchema' xmlns:xsi='http://www.w3.org/2001/XMLSchema-instance'>
<soap:Body>
<InjectUAVControllerInterface><a>1</a><b>2</b></InjectUAVControllerInterface>
</soap:Body>
</soap:Envelope>)");
        free(reply);
        activation_frame_counter = frame_counter;
        controller_started = true;
    }

    float scaled_servos[8];
    for (uint8_t i=0; i<8; i++) {
        scaled_servos[i] = (input.servos[i] - 1000) / 1000.0f;
    }

    if (rev4_servos) {
        // swap first 4 and last 4 servos, for quadplane testing
        float saved[4];
        memcpy(saved, &scaled_servos[0], sizeof(saved));
        memcpy(&scaled_servos[0], &scaled_servos[4], sizeof(saved));
        memcpy(&scaled_servos[4], saved, sizeof(saved));
    }

    if (heli_demix) {
        // FlightAxis expects "roll/pitch/collective/yaw" input
        float swash1 = scaled_servos[0];
        float swash2 = scaled_servos[1];
        float swash3 = scaled_servos[2];

        float roll_rate = swash1 - swash2;
        float pitch_rate = -((swash1+swash2) / 2.0f - swash3);

        scaled_servos[0] = constrain_float(roll_rate + 0.5, 0, 1);
        scaled_servos[1] = constrain_float(pitch_rate + 0.5, 0, 1);
    }


    char *reply = soap_request("ExchangeData", R"(<?xml version='1.0' encoding='UTF-8'?><soap:Envelope xmlns:soap='http://schemas.xmlsoap.org/soap/envelope/' xmlns:xsd='http://www.w3.org/2001/XMLSchema' xmlns:xsi='http://www.w3.org/2001/XMLSchema-instance'>
<soap:Body>
<ExchangeData>
<pControlInputs>
<m-selectedChannels>255</m-selectedChannels>
<m-channelValues-0to1>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
</m-channelValues-0to1>
</pControlInputs>
</ExchangeData>
</soap:Body>
</soap:Envelope>)",
                               scaled_servos[0],
                               scaled_servos[1],
                               scaled_servos[2],
                               scaled_servos[3],
                               scaled_servos[4],
                               scaled_servos[5],
                               scaled_servos[6],
                               scaled_servos[7]);

    if (reply) {
        parse_reply(reply);
        free(reply);
    }
}


/*
  update the FlightAxis simulation by one time step
 */
void FlightAxis::update(const struct sitl_input &input)
{
    exchange_data(input);

    double dt_seconds = state.m_currentPhysicsTime_SEC - last_time_s;
    if (dt_seconds < 0) {
        // cope with restarting RealFlight while connected
        initial_time_s = time_now_us * 1.0e-6f;
        last_time_s = state.m_currentPhysicsTime_SEC;
        position_offset.zero();
        return;
    }
    if (dt_seconds < 0.0001f) {
        // we probably got a repeated frame
        time_now_us += 1;
        return;
    }
    if (initial_time_s <= 0) {
        dt_seconds = 0.001f;
        initial_time_s = state.m_currentPhysicsTime_SEC - dt_seconds;
    }

    /*
      the queternion convention in realflight seems to have Z negative
     */
    Quaternion quat(state.m_orientationQuaternion_W,
                    state.m_orientationQuaternion_Y,
                    state.m_orientationQuaternion_X,
                    -state.m_orientationQuaternion_Z);
    quat.rotation_matrix(dcm);

    gyro = Vector3f(radians(constrain_float(state.m_rollRate_DEGpSEC, -2000, 2000)),
                    radians(constrain_float(state.m_pitchRate_DEGpSEC, -2000, 2000)),
                    -radians(constrain_float(state.m_yawRate_DEGpSEC, -2000, 2000))) * target_speedup;

    velocity_ef = Vector3f(state.m_velocityWorldU_MPS,
                             state.m_velocityWorldV_MPS,
                             state.m_velocityWorldW_MPS);
    position = Vector3f(state.m_aircraftPositionY_MTR,
                        state.m_aircraftPositionX_MTR,
                        -state.m_altitudeASL_MTR - home.alt*0.01);

    accel_body(state.m_accelerationBodyAX_MPS2,
               state.m_accelerationBodyAY_MPS2,
               state.m_accelerationBodyAZ_MPS2);

    if (rotation != ROTATION_NONE) {
        dcm.transpose();
        dcm = att_rotation * dcm;
        dcm.transpose();
        gyro.rotate(rotation);
        accel_body.rotate(rotation);
    }

    // accel on the ground is nasty in realflight, and prevents helicopter disarm
    if (state.m_isTouchingGround) {
        Vector3f accel_ef = (velocity_ef - last_velocity_ef) / dt_seconds;
        accel_ef.z -= GRAVITY_MSS;
        accel_body = dcm.transposed() * accel_ef;
    }

    // limit to 16G to match pixhawk
    float a_limit = GRAVITY_MSS*16;
    accel_body.x = constrain_float(accel_body.x, -a_limit, a_limit);
    accel_body.y = constrain_float(accel_body.y, -a_limit, a_limit);
    accel_body.z = constrain_float(accel_body.z, -a_limit, a_limit);

    // offset based on first position to account for offset in RF world
    if (position_offset.is_zero() || state.m_resetButtonHasBeenPressed) {
        position_offset = position;
    }
    position -= position_offset;

    airspeed = state.m_airspeed_MPS;
    airspeed_pitot = state.m_airspeed_MPS;

    battery_voltage = state.m_batteryVoltage_VOLTS;
    battery_current = state.m_batteryCurrentDraw_AMPS;
    rpm1 = state.m_heliMainRotorRPM;
    rpm2 = state.m_propRPM;

    /*
      the interlink interface supports 8 input channels
     */
    rcin_chan_count = 8;
    for (uint8_t i=0; i<rcin_chan_count; i++) {
        rcin[i] = state.rcin[i];
    }

    update_position();
    time_advance();
    time_now_us = (state.m_currentPhysicsTime_SEC - initial_time_s)*1.0e6;

    if (frame_counter++ % 1000 == 0) {
        if (last_frame_count_s != 0) {
            printf("%.2f FPS\n",
                   1000 / (state.m_currentPhysicsTime_SEC - last_frame_count_s));
        } else {
            printf("Initial position %f %f %f\n", position.x, position.y, position.z);
        }
        last_frame_count_s = state.m_currentPhysicsTime_SEC;
    }

    last_time_s = state.m_currentPhysicsTime_SEC;

    last_velocity_ef = velocity_ef;

    // update magnetic field
    update_mag_field_bf();
}

} // namespace SITL