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https://github.com/ArduPilot/ardupilot
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SITL: support AHRS_ORIENTATION in SITL
this allows for tailsitters in RealFlight
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@ -73,11 +73,10 @@ Aircraft::Aircraft(const char *home_str, const char *frame_str) :
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last_wall_time_us = get_wall_time_us();
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frame_counter = 0;
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// support rotated IMUs for testing
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if (strstr(frame_str, "-roll180")) {
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imu_rotation = ROTATION_ROLL_180;
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}
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// allow for orientation settings, such as with tailsitters
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enum ap_var_type ptype;
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ahrs_orientation = (AP_Int8 *)AP_Param::find("AHRS_ORIENTATION", &ptype);
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terrain = (AP_Terrain *)AP_Param::find_object("TERRAIN_");
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}
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@ -392,18 +391,21 @@ void Aircraft::fill_fdm(struct sitl_fdm &fdm)
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fdm.altitude = smoothing.location.alt * 1.0e-2;
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}
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if (imu_rotation != ROTATION_NONE) {
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Vector3f accel(fdm.xAccel, fdm.yAccel, fdm.zAccel);
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accel.rotate(imu_rotation);
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fdm.xAccel = accel.x;
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fdm.yAccel = accel.y;
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fdm.zAccel = accel.z;
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if (ahrs_orientation != nullptr) {
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enum Rotation imu_rotation = (enum Rotation)ahrs_orientation->get();
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Vector3f rgyro(fdm.rollRate, fdm.pitchRate, fdm.yawRate);
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rgyro.rotate(imu_rotation);
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fdm.rollRate = degrees(rgyro.x);
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fdm.pitchRate = degrees(rgyro.y);
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fdm.yawRate = degrees(rgyro.z);
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if (imu_rotation != ROTATION_NONE) {
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Matrix3f m = dcm;
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Matrix3f rot;
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rot.from_rotation(imu_rotation);
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m = m * rot.transposed();
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m.to_euler(&r, &p, &y);
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fdm.rollDeg = degrees(r);
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fdm.pitchDeg = degrees(p);
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fdm.yawDeg = degrees(y);
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fdm.quaternion.from_rotation_matrix(m);
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}
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}
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if (last_speedup != sitl->speedup && sitl->speedup > 0) {
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@ -164,8 +164,9 @@ protected:
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bool use_time_sync = true;
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float last_speedup = -1.0f;
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enum Rotation imu_rotation = ROTATION_NONE;
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// allow for AHRS_ORIENTATION
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AP_Int8 *ahrs_orientation;
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enum {
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GROUND_BEHAVIOR_NONE = 0,
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GROUND_BEHAVIOR_NO_MOVEMENT,
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@ -87,28 +87,6 @@ FlightAxis::FlightAxis(const char *home_str, const char *frame_str) :
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AP_Param::set_default_by_name(sim_defaults[i].name, sim_defaults[i].value);
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}
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if (strstr(frame_str, "pitch270")) {
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// rotate tailsitter airframes for fixed wing view
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rotation = ROTATION_PITCH_270;
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}
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if (strstr(frame_str, "pitch90")) {
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// rotate tailsitter airframes for fixed wing view
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rotation = ROTATION_PITCH_90;
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}
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switch (rotation) {
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case ROTATION_NONE:
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break;
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case ROTATION_PITCH_90:
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att_rotation.from_euler(0, radians(90), 0);
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break;
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case ROTATION_PITCH_270:
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att_rotation.from_euler(0, radians(270), 0);
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break;
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default:
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AP_HAL::panic("Unsupported flightaxis rotation %u\n", (unsigned)rotation);
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}
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/* Create the thread that will be waiting for data from FlightAxis */
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mutex = hal.util->new_semaphore();
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@ -428,14 +406,6 @@ void FlightAxis::update(const struct sitl_input &input)
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state.m_accelerationBodyAY_MPS2,
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state.m_accelerationBodyAZ_MPS2);
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if (rotation != ROTATION_NONE) {
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dcm.transpose();
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dcm = att_rotation * dcm;
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dcm.transpose();
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gyro.rotate(rotation);
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accel_body.rotate(rotation);
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}
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// accel on the ground is nasty in realflight, and prevents helicopter disarm
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if (state.m_isTouchingGround) {
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Vector3f accel_ef = (velocity_ef - last_velocity_ef) / dt_seconds;
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@ -176,8 +176,6 @@ private:
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double last_frame_count_s;
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Vector3f position_offset;
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Vector3f last_velocity_ef;
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Matrix3f att_rotation;
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enum Rotation rotation = ROTATION_NONE;
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const char *controller_ip = "127.0.0.1";
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uint16_t controller_port = 18083;
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