ardupilot/ArduPlane/GCS_Mavlink.cpp

#include "GCS_Mavlink.h"

#include "Plane.h"
#include <AP_RPM/AP_RPM_config.h>
#include <AP_Airspeed/AP_Airspeed_config.h>
#include <AP_EFI/AP_EFI_config.h>

MAV_TYPE GCS_Plane::frame_type() const
{
#if HAL_QUADPLANE_ENABLED
    return plane.quadplane.get_mav_type();
#else
    return MAV_TYPE_FIXED_WING;
#endif
}

MAV_MODE GCS_MAVLINK_Plane::base_mode() const
{
    uint8_t _base_mode = MAV_MODE_FLAG_CUSTOM_MODE_ENABLED;

    // work out the base_mode. This value is not very useful
    // for APM, but we calculate it as best we can so a generic
    // MAVLink enabled ground station can work out something about
    // what the MAV is up to. The actual bit values are highly
    // ambiguous for most of the APM flight modes. In practice, you
    // only get useful information from the custom_mode, which maps to
    // the APM flight mode and has a well defined meaning in the
    // ArduPlane documentation
    switch (plane.control_mode->mode_number()) {
    case Mode::Number::MANUAL:
    case Mode::Number::TRAINING:
    case Mode::Number::ACRO:
#if HAL_QUADPLANE_ENABLED
    case Mode::Number::QACRO:
        _base_mode = MAV_MODE_FLAG_MANUAL_INPUT_ENABLED;
        break;
#endif
    case Mode::Number::STABILIZE:
    case Mode::Number::FLY_BY_WIRE_A:
    case Mode::Number::AUTOTUNE:
    case Mode::Number::FLY_BY_WIRE_B:
#if HAL_QUADPLANE_ENABLED
    case Mode::Number::QSTABILIZE:
    case Mode::Number::QHOVER:
    case Mode::Number::QLOITER:
    case Mode::Number::QLAND:
#if QAUTOTUNE_ENABLED
    case Mode::Number::QAUTOTUNE:
#endif
#endif  // HAL_QUADPLANE_ENABLED
    case Mode::Number::CRUISE:
        _base_mode = MAV_MODE_FLAG_STABILIZE_ENABLED;
        break;
    case Mode::Number::AUTO:
    case Mode::Number::RTL:
    case Mode::Number::LOITER:
    case Mode::Number::THERMAL:
    case Mode::Number::AVOID_ADSB:
    case Mode::Number::GUIDED:
    case Mode::Number::CIRCLE:
    case Mode::Number::TAKEOFF:
#if HAL_QUADPLANE_ENABLED
    case Mode::Number::QRTL:
    case Mode::Number::LOITER_ALT_QLAND:
#endif
        _base_mode = MAV_MODE_FLAG_GUIDED_ENABLED |
                     MAV_MODE_FLAG_STABILIZE_ENABLED;
        // note that MAV_MODE_FLAG_AUTO_ENABLED does not match what
        // APM does in any mode, as that is defined as "system finds its own goal
        // positions", which APM does not currently do
        break;
    case Mode::Number::INITIALISING:
        break;
    }

    if (!plane.training_manual_pitch || !plane.training_manual_roll) {
        _base_mode |= MAV_MODE_FLAG_STABILIZE_ENABLED;        
    }

    if (plane.control_mode != &plane.mode_manual && plane.control_mode != &plane.mode_initializing) {
        // stabiliser of some form is enabled
        _base_mode |= MAV_MODE_FLAG_STABILIZE_ENABLED;
    }

    if (plane.g.stick_mixing != StickMixing::NONE && plane.control_mode != &plane.mode_initializing) {
        if ((plane.g.stick_mixing != StickMixing::VTOL_YAW) || (plane.control_mode == &plane.mode_auto)) {
            // all modes except INITIALISING have some form of manual
            // override if stick mixing is enabled
            _base_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED;
        }
    }

    // we are armed if we are not initialising
    if (plane.control_mode != &plane.mode_initializing && plane.arming.is_armed()) {
        _base_mode |= MAV_MODE_FLAG_SAFETY_ARMED;
    }

    // indicate we have set a custom mode
    _base_mode |= MAV_MODE_FLAG_CUSTOM_MODE_ENABLED;

    return (MAV_MODE)_base_mode;
}

uint32_t GCS_Plane::custom_mode() const
{
    return plane.control_mode->mode_number();
}

MAV_STATE GCS_MAVLINK_Plane::vehicle_system_status() const
{
    if (plane.control_mode == &plane.mode_initializing) {
        return MAV_STATE_CALIBRATING;
    }
    if (plane.any_failsafe_triggered()) {
        return MAV_STATE_CRITICAL;
    }
    if (plane.crash_state.is_crashed) {
        return MAV_STATE_EMERGENCY;
    }
    if (plane.is_flying()) {
        return MAV_STATE_ACTIVE;
    }

    return MAV_STATE_STANDBY;
}


void GCS_MAVLINK_Plane::send_attitude() const
{
    const AP_AHRS &ahrs = AP::ahrs();

    float r = ahrs.roll;
    float p = ahrs.pitch;
    float y = ahrs.yaw;

    if (!(plane.g2.flight_options & FlightOptions::GCS_REMOVE_TRIM_PITCH_CD)) {
        p -= radians(plane.g.pitch_trim_cd * 0.01f);
    }

#if HAL_QUADPLANE_ENABLED
    if (plane.quadplane.show_vtol_view()) {
        r = plane.quadplane.ahrs_view->roll;
        p = plane.quadplane.ahrs_view->pitch;
        y = plane.quadplane.ahrs_view->yaw;
    }
#endif

    const Vector3f &omega = ahrs.get_gyro();
    mavlink_msg_attitude_send(
        chan,
        millis(),
        r,
        p,
        y,
        omega.x,
        omega.y,
        omega.z);
}

void GCS_MAVLINK_Plane::send_aoa_ssa()
{
    AP_AHRS &ahrs = AP::ahrs();

    mavlink_msg_aoa_ssa_send(
        chan,
        micros(),
        ahrs.getAOA(),
        ahrs.getSSA());
}

void GCS_MAVLINK_Plane::send_nav_controller_output() const
{
    if (plane.control_mode == &plane.mode_manual) {
        return;
    }
#if HAL_QUADPLANE_ENABLED
    const QuadPlane &quadplane = plane.quadplane;
    if (quadplane.show_vtol_view() && quadplane.using_wp_nav()) {
        const Vector3f &targets = quadplane.attitude_control->get_att_target_euler_cd();

        const Vector2f& curr_pos = quadplane.inertial_nav.get_position_xy_cm();
        const Vector2f& target_pos = quadplane.pos_control->get_pos_target_cm().xy().tofloat();
        const Vector2f error = (target_pos - curr_pos) * 0.01;

        mavlink_msg_nav_controller_output_send(
            chan,
            targets.x * 0.01,
            targets.y * 0.01,
            targets.z * 0.01,
            degrees(error.angle()),
            MIN(error.length(), UINT16_MAX),
            (plane.control_mode != &plane.mode_qstabilize) ? quadplane.pos_control->get_pos_error_z_cm() * 0.01 : 0,
            plane.airspeed_error * 100,  // incorrect units; see PR#7933
            quadplane.wp_nav->crosstrack_error());
        return;
    }
#endif
    {
        const AP_Navigation *nav_controller = plane.nav_controller;
        mavlink_msg_nav_controller_output_send(
            chan,
            plane.nav_roll_cd * 0.01,
            plane.nav_pitch_cd * 0.01,
            nav_controller->nav_bearing_cd() * 0.01,
            nav_controller->target_bearing_cd() * 0.01,
            MIN(plane.auto_state.wp_distance, UINT16_MAX),
            plane.altitude_error_cm * 0.01,
            plane.airspeed_error * 100,  // incorrect units; see PR#7933
            nav_controller->crosstrack_error());
    }
}

void GCS_MAVLINK_Plane::send_position_target_global_int()
{
    if (plane.control_mode == &plane.mode_manual) {
        return;
    }
    Location &next_WP_loc = plane.next_WP_loc;
    static constexpr uint16_t POSITION_TARGET_TYPEMASK_LAST_BYTE = 0xF000;
    static constexpr uint16_t TYPE_MASK = POSITION_TARGET_TYPEMASK_VX_IGNORE | POSITION_TARGET_TYPEMASK_VY_IGNORE | POSITION_TARGET_TYPEMASK_VZ_IGNORE |
                                          POSITION_TARGET_TYPEMASK_AX_IGNORE | POSITION_TARGET_TYPEMASK_AY_IGNORE | POSITION_TARGET_TYPEMASK_AZ_IGNORE |
                                          POSITION_TARGET_TYPEMASK_YAW_IGNORE | POSITION_TARGET_TYPEMASK_YAW_RATE_IGNORE | POSITION_TARGET_TYPEMASK_LAST_BYTE;
    int32_t alt = 0;
    if (!next_WP_loc.is_zero()) {
        UNUSED_RESULT(next_WP_loc.get_alt_cm(Location::AltFrame::ABSOLUTE, alt));
    }

    mavlink_msg_position_target_global_int_send(
        chan,
        AP_HAL::millis(), // time_boot_ms
        MAV_FRAME_GLOBAL, // targets are always global altitude
        TYPE_MASK, // ignore everything except the x/y/z components
        next_WP_loc.lat, // latitude as 1e7
        next_WP_loc.lng, // longitude as 1e7
        alt * 0.01, // altitude is sent as a float
        0.0f, // vx
        0.0f, // vy
        0.0f, // vz
        0.0f, // afx
        0.0f, // afy
        0.0f, // afz
        0.0f, // yaw
        0.0f); // yaw_rate
}


float GCS_MAVLINK_Plane::vfr_hud_airspeed() const
{
    // airspeed sensors are best.  While the AHRS airspeed_estimate
    // will use an airspeed sensor, that value is constrained by the
    // ground speed.  When reporting we should send the true airspeed
    // value if possible:
#if AP_AIRSPEED_ENABLED
    if (plane.airspeed.enabled() && plane.airspeed.healthy()) {
        return plane.airspeed.get_airspeed();
    }
#endif

    // airspeed estimates are OK:
    float aspeed;
    if (AP::ahrs().airspeed_estimate(aspeed)) {
        return aspeed;
    }

    // lying is worst:
    return 0;
}

int16_t GCS_MAVLINK_Plane::vfr_hud_throttle() const
{
    return plane.throttle_percentage();
}

float GCS_MAVLINK_Plane::vfr_hud_climbrate() const
{
#if HAL_SOARING_ENABLED
    if (plane.g2.soaring_controller.is_active()) {
        return plane.g2.soaring_controller.get_vario_reading();
    }
#endif
    return GCS_MAVLINK::vfr_hud_climbrate();
}

void GCS_MAVLINK_Plane::send_wind() const
{
    const Vector3f wind = AP::ahrs().wind_estimate();
    mavlink_msg_wind_send(
        chan,
        degrees(atan2f(-wind.y, -wind.x)), // use negative, to give
                                          // direction wind is coming from
        wind.length(),
        wind.z);
}

// sends a single pid info over the provided channel
void GCS_MAVLINK_Plane::send_pid_info(const AP_PIDInfo *pid_info,
                          const uint8_t axis, const float achieved)
{
    if (pid_info == nullptr) {
        return;
    }
    if (!HAVE_PAYLOAD_SPACE(chan, PID_TUNING)) {
        return;
    }
     mavlink_msg_pid_tuning_send(chan, axis,
                                 pid_info->target,
                                 achieved,
                                 pid_info->FF,
                                 pid_info->P,
                                 pid_info->I,
                                 pid_info->D,
                                 pid_info->slew_rate,
                                 pid_info->Dmod);
}

/*
  send PID tuning message
 */
void GCS_MAVLINK_Plane::send_pid_tuning()
{
    if (plane.control_mode == &plane.mode_manual) {
        // no PIDs should be used in manual
        return;
    }

    const Parameters &g = plane.g;

    const AP_PIDInfo *pid_info;
    if (g.gcs_pid_mask & TUNING_BITS_ROLL) {
        pid_info = &plane.rollController.get_pid_info();
#if HAL_QUADPLANE_ENABLED
        if (plane.quadplane.in_vtol_mode()) {
            pid_info = &plane.quadplane.attitude_control->get_rate_roll_pid().get_pid_info();
        }
#endif
        send_pid_info(pid_info, PID_TUNING_ROLL, pid_info->actual);
    }
    if (g.gcs_pid_mask & TUNING_BITS_PITCH) {
        pid_info = &plane.pitchController.get_pid_info();
#if HAL_QUADPLANE_ENABLED
        if (plane.quadplane.in_vtol_mode()) {
            pid_info = &plane.quadplane.attitude_control->get_rate_pitch_pid().get_pid_info();
        }
#endif
        send_pid_info(pid_info, PID_TUNING_PITCH, pid_info->actual);
    }
    if (g.gcs_pid_mask & TUNING_BITS_YAW) {
        pid_info = &plane.yawController.get_pid_info();
#if HAL_QUADPLANE_ENABLED
        if (plane.quadplane.in_vtol_mode()) {
            pid_info = &plane.quadplane.attitude_control->get_rate_yaw_pid().get_pid_info();
        }
#endif
        send_pid_info(pid_info, PID_TUNING_YAW, pid_info->actual);
    }
    if (g.gcs_pid_mask & TUNING_BITS_STEER) {
        pid_info = &plane.steerController.get_pid_info();
        send_pid_info(pid_info, PID_TUNING_STEER, pid_info->actual);
    }
    if ((g.gcs_pid_mask & TUNING_BITS_LAND) && (plane.flight_stage == AP_FixedWing::FlightStage::LAND)) {
        AP_AHRS &ahrs = AP::ahrs();
        const Vector3f &gyro = ahrs.get_gyro();
        send_pid_info(plane.landing.get_pid_info(), PID_TUNING_LANDING, degrees(gyro.z));
    }
#if HAL_QUADPLANE_ENABLED
    if (g.gcs_pid_mask & TUNING_BITS_ACCZ && plane.quadplane.in_vtol_mode()) {
        pid_info = &plane.quadplane.pos_control->get_accel_z_pid().get_pid_info();
        send_pid_info(pid_info, PID_TUNING_ACCZ, pid_info->actual);
    }
#endif
 }

uint8_t GCS_MAVLINK_Plane::sysid_my_gcs() const
{
    return plane.g.sysid_my_gcs;
}
bool GCS_MAVLINK_Plane::sysid_enforce() const
{
    return plane.g2.sysid_enforce;
}

uint32_t GCS_MAVLINK_Plane::telem_delay() const
{
    return (uint32_t)(plane.g.telem_delay);
}

// try to send a message, return false if it won't fit in the serial tx buffer
bool GCS_MAVLINK_Plane::try_send_message(enum ap_message id)
{
    switch (id) {

    case MSG_SERVO_OUT:
        // unused
        break;

    case MSG_TERRAIN:
#if AP_TERRAIN_AVAILABLE
        CHECK_PAYLOAD_SIZE(TERRAIN_REQUEST);
        plane.terrain.send_request(chan);
#endif
        break;

    case MSG_WIND:
        CHECK_PAYLOAD_SIZE(WIND);
        send_wind();
        break;

    case MSG_ADSB_VEHICLE:
#if HAL_ADSB_ENABLED
        CHECK_PAYLOAD_SIZE(ADSB_VEHICLE);
        plane.adsb.send_adsb_vehicle(chan);
#endif
        break;

    case MSG_AOA_SSA:
        CHECK_PAYLOAD_SIZE(AOA_SSA);
        send_aoa_ssa();
        break;
    case MSG_LANDING:
        plane.landing.send_landing_message(chan);
        break;

    case MSG_HYGROMETER:
#if AP_AIRSPEED_HYGROMETER_ENABLE
        CHECK_PAYLOAD_SIZE(HYGROMETER_SENSOR);
        send_hygrometer();
#endif
        break;

    default:
        return GCS_MAVLINK::try_send_message(id);
    }
    return true;
}

#if AP_AIRSPEED_HYGROMETER_ENABLE
void GCS_MAVLINK_Plane::send_hygrometer()
{
    if (!HAVE_PAYLOAD_SPACE(chan, HYGROMETER_SENSOR)) {
        return;
    }

    const auto *airspeed = AP::airspeed();
    if (airspeed == nullptr) {
        return;
    } 
    const uint32_t now = AP_HAL::millis();

    for (uint8_t i=0; i<AIRSPEED_MAX_SENSORS; i++) {
        uint8_t idx = (i+last_hygrometer_send_idx+1) % AIRSPEED_MAX_SENSORS;
        float temperature, humidity;
        uint32_t last_sample_ms;
        if (!airspeed->get_hygrometer(idx, last_sample_ms, temperature, humidity)) {
            continue;
        }
        if (now - last_sample_ms > 2000) {
            // not updating, stop sending
            continue;
        }
        if (!HAVE_PAYLOAD_SPACE(chan, HYGROMETER_SENSOR)) {
            return;
        }

        mavlink_msg_hygrometer_sensor_send(
            chan,
            idx,
            int16_t(temperature*100),
            uint16_t(humidity*100));
        last_hygrometer_send_idx = idx;
    }
}
#endif // AP_AIRSPEED_HYGROMETER_ENABLE


/*
  default stream rates to 1Hz
 */
const AP_Param::GroupInfo GCS_MAVLINK_Parameters::var_info[] = {
    // @Param: RAW_SENS
    // @DisplayName: Raw sensor stream rate
    // @Description: MAVLink Stream rate of RAW_IMU, SCALED_IMU2, SCALED_IMU3, SCALED_PRESSURE, SCALED_PRESSURE2, and SCALED_PRESSURE3
    // @Units: Hz
    // @Range: 0 50
    // @Increment: 1
    // @RebootRequired: True
    // @User: Advanced
    AP_GROUPINFO("RAW_SENS", 0, GCS_MAVLINK_Parameters, streamRates[0],  1),

    // @Param: EXT_STAT
    // @DisplayName: Extended status stream rate
    // @Description: MAVLink Stream rate of SYS_STATUS, POWER_STATUS, MCU_STATUS, MEMINFO, CURRENT_WAYPOINT, GPS_RAW_INT, GPS_RTK (if available), GPS2_RAW_INT (if available), GPS2_RTK (if available), NAV_CONTROLLER_OUTPUT, FENCE_STATUS, and GLOBAL_TARGET_POS_INT
    // @Units: Hz
    // @Range: 0 50
    // @Increment: 1
    // @RebootRequired: True
    // @User: Advanced
    AP_GROUPINFO("EXT_STAT", 1, GCS_MAVLINK_Parameters, streamRates[1],  1),

    // @Param: RC_CHAN
    // @DisplayName: RC Channel stream rate
    // @Description: MAVLink Stream rate of SERVO_OUTPUT_RAW and RC_CHANNELS
    // @Units: Hz
    // @Range: 0 50
    // @Increment: 1
    // @RebootRequired: True
    // @User: Advanced
    AP_GROUPINFO("RC_CHAN",  2, GCS_MAVLINK_Parameters, streamRates[2],  1),

    // @Param: RAW_CTRL
    // @DisplayName: Raw Control stream rate
    // @Description: MAVLink Raw Control stream rate of SERVO_OUT
    // @Units: Hz
    // @Range: 0 50
    // @Increment: 1
    // @RebootRequired: True
    // @User: Advanced
    AP_GROUPINFO("RAW_CTRL", 3, GCS_MAVLINK_Parameters, streamRates[3],  1),

    // @Param: POSITION
    // @DisplayName: Position stream rate
    // @Description: MAVLink Stream rate of GLOBAL_POSITION_INT and LOCAL_POSITION_NED
    // @Units: Hz
    // @Range: 0 50
    // @Increment: 1
    // @RebootRequired: True
    // @User: Advanced
    AP_GROUPINFO("POSITION", 4, GCS_MAVLINK_Parameters, streamRates[4],  1),

    // @Param: EXTRA1
    // @DisplayName: Extra data type 1 stream rate
    // @Description: MAVLink Stream rate of ATTITUDE, SIMSTATE (SIM only), AHRS2, RPM, AOA_SSA, LANDING,ESC_TELEMETRY,EFI_STATUS, and PID_TUNING
    // @Units: Hz
    // @Range: 0 50
    // @Increment: 1
    // @RebootRequired: True
    // @User: Advanced
    AP_GROUPINFO("EXTRA1",   5, GCS_MAVLINK_Parameters, streamRates[5],  1),

    // @Param: EXTRA2
    // @DisplayName: Extra data type 2 stream rate
    // @Description: MAVLink Stream rate of VFR_HUD
    // @Range: 0 50
    // @Increment: 1
    // @RebootRequired: True
    // @User: Advanced
    AP_GROUPINFO("EXTRA2",   6, GCS_MAVLINK_Parameters, streamRates[6],  1),

    // @Param: EXTRA3
    // @DisplayName: Extra data type 3 stream rate
    // @Description: MAVLink Stream rate of AHRS, SYSTEM_TIME, WIND, RANGEFINDER, DISTANCE_SENSOR, TERRAIN_REQUEST, BATTERY2, GIMBAL_DEVICE_ATTITUDE_STATUS, OPTICAL_FLOW, MAG_CAL_REPORT, MAG_CAL_PROGRESS, EKF_STATUS_REPORT, VIBRATION, and BATTERY_STATUS
    // @Units: Hz
    // @Range: 0 50
    // @Increment: 1
    // @RebootRequired: True
    // @User: Advanced
    AP_GROUPINFO("EXTRA3",   7, GCS_MAVLINK_Parameters, streamRates[7],  1),

    // @Param: PARAMS
    // @DisplayName: Parameter stream rate
    // @Description: MAVLink Stream rate of PARAM_VALUE
    // @Units: Hz
    // @Range: 0 50
    // @Increment: 1
    // @RebootRequired: True
    // @User: Advanced
    AP_GROUPINFO("PARAMS",   8, GCS_MAVLINK_Parameters, streamRates[8],  10),

    // @Param: ADSB
    // @DisplayName: ADSB stream rate
    // @Description: MAVLink ADSB stream rate
    // @Units: Hz
    // @Range: 0 50
    // @Increment: 1
    // @RebootRequired: True
    // @User: Advanced
    AP_GROUPINFO("ADSB",   9, GCS_MAVLINK_Parameters, streamRates[9],  5),
    AP_GROUPEND
};

static const ap_message STREAM_RAW_SENSORS_msgs[] = {
    MSG_RAW_IMU,
    MSG_SCALED_IMU2,
    MSG_SCALED_IMU3,
    MSG_SCALED_PRESSURE,
    MSG_SCALED_PRESSURE2,
    MSG_SCALED_PRESSURE3,
};
static const ap_message STREAM_EXTENDED_STATUS_msgs[] = {
    MSG_SYS_STATUS,
    MSG_POWER_STATUS,
    MSG_MCU_STATUS,
    MSG_MEMINFO,
    MSG_CURRENT_WAYPOINT,
    MSG_GPS_RAW,
    MSG_GPS_RTK,
    MSG_GPS2_RAW,
    MSG_GPS2_RTK,
    MSG_NAV_CONTROLLER_OUTPUT,
    MSG_FENCE_STATUS,
    MSG_POSITION_TARGET_GLOBAL_INT,
};
static const ap_message STREAM_POSITION_msgs[] = {
    MSG_LOCATION,
    MSG_LOCAL_POSITION
};
static const ap_message STREAM_RAW_CONTROLLER_msgs[] = {
    MSG_SERVO_OUT,
};
static const ap_message STREAM_RC_CHANNELS_msgs[] = {
    MSG_SERVO_OUTPUT_RAW,
    MSG_RC_CHANNELS,
    MSG_RC_CHANNELS_RAW, // only sent on a mavlink1 connection
};
static const ap_message STREAM_EXTRA1_msgs[] = {
    MSG_ATTITUDE,
    MSG_SIMSTATE,
    MSG_AHRS2,
#if AP_RPM_ENABLED
    MSG_RPM,
#endif
    MSG_AOA_SSA,
    MSG_PID_TUNING,
    MSG_LANDING,
    MSG_ESC_TELEMETRY,
#if HAL_EFI_ENABLED
    MSG_EFI_STATUS,
#endif
#if AP_AIRSPEED_HYGROMETER_ENABLE
    MSG_HYGROMETER,
#endif
};
static const ap_message STREAM_EXTRA2_msgs[] = {
    MSG_VFR_HUD
};
static const ap_message STREAM_EXTRA3_msgs[] = {
    MSG_AHRS,
    MSG_WIND,
    MSG_RANGEFINDER,
    MSG_DISTANCE_SENSOR,
    MSG_SYSTEM_TIME,
#if AP_TERRAIN_AVAILABLE
    MSG_TERRAIN,
#endif
    MSG_BATTERY_STATUS,
    MSG_GIMBAL_DEVICE_ATTITUDE_STATUS,
    MSG_OPTICAL_FLOW,
    MSG_MAG_CAL_REPORT,
    MSG_MAG_CAL_PROGRESS,
    MSG_EKF_STATUS_REPORT,
    MSG_VIBRATION,
};
static const ap_message STREAM_PARAMS_msgs[] = {
    MSG_NEXT_PARAM
};
static const ap_message STREAM_ADSB_msgs[] = {
    MSG_ADSB_VEHICLE,
    MSG_AIS_VESSEL,
};

const struct GCS_MAVLINK::stream_entries GCS_MAVLINK::all_stream_entries[] = {
    MAV_STREAM_ENTRY(STREAM_RAW_SENSORS),
    MAV_STREAM_ENTRY(STREAM_EXTENDED_STATUS),
    MAV_STREAM_ENTRY(STREAM_POSITION),
    MAV_STREAM_ENTRY(STREAM_RAW_CONTROLLER),
    MAV_STREAM_ENTRY(STREAM_RC_CHANNELS),
    MAV_STREAM_ENTRY(STREAM_EXTRA1),
    MAV_STREAM_ENTRY(STREAM_EXTRA2),
    MAV_STREAM_ENTRY(STREAM_EXTRA3),
    MAV_STREAM_ENTRY(STREAM_PARAMS),
    MAV_STREAM_ENTRY(STREAM_ADSB),
    MAV_STREAM_TERMINATOR // must have this at end of stream_entries
};

/*
  handle a request to switch to guided mode. This happens via a
  callback from handle_mission_item()
 */
bool GCS_MAVLINK_Plane::handle_guided_request(AP_Mission::Mission_Command &cmd)
{
    return plane.control_mode->handle_guided_request(cmd.content.location);
}

/*
  handle a request to change current WP altitude. This happens via a
  callback from handle_mission_item()
 */
void GCS_MAVLINK_Plane::handle_change_alt_request(AP_Mission::Mission_Command &cmd)
{
    plane.next_WP_loc.alt = cmd.content.location.alt;
    if (cmd.content.location.relative_alt) {
        plane.next_WP_loc.alt += plane.home.alt;
    }
    plane.next_WP_loc.relative_alt = false;
    plane.next_WP_loc.terrain_alt = cmd.content.location.terrain_alt;
    plane.reset_offset_altitude();
}


MAV_RESULT GCS_MAVLINK_Plane::handle_command_preflight_calibration(const mavlink_command_long_t &packet)
{
    plane.in_calibration = true;
    MAV_RESULT ret = GCS_MAVLINK::handle_command_preflight_calibration(packet);
    plane.in_calibration = false;

    return ret;
}

void GCS_MAVLINK_Plane::packetReceived(const mavlink_status_t &status,
                                       const mavlink_message_t &msg)
{
#if HAL_ADSB_ENABLED
    plane.avoidance_adsb.handle_msg(msg);
#endif
#if AP_SCRIPTING_ENABLED
    // pass message to follow library
    plane.g2.follow.handle_msg(msg);
#endif
    GCS_MAVLINK::packetReceived(status, msg);
}


bool GCS_MAVLINK_Plane::set_home_to_current_location(bool _lock)
{
    if (!plane.set_home_persistently(AP::gps().location())) {
        return false;
    }
    if (_lock) {
        AP::ahrs().lock_home();
    }
    return true;
}
bool GCS_MAVLINK_Plane::set_home(const Location& loc, bool _lock)
{
    if (!AP::ahrs().set_home(loc)) {
        return false;
    }
    if (_lock) {
        AP::ahrs().lock_home();
    }
    return true;
}

MAV_RESULT GCS_MAVLINK_Plane::handle_command_int_do_reposition(const mavlink_command_int_t &packet)
{
    // sanity check location
    if (!check_latlng(packet.x, packet.y)) {
        return MAV_RESULT_DENIED;
    }

    Location requested_position;
    if (!location_from_command_t(packet, requested_position)) {
        return MAV_RESULT_DENIED;
    }

    if (is_zero(packet.param4)) {
        requested_position.loiter_ccw = 0;
    } else {
        requested_position.loiter_ccw = 1;
    }

    if (requested_position.sanitize(plane.current_loc)) {
        // if the location wasn't already sane don't load it
        return MAV_RESULT_DENIED;
    }

    // location is valid load and set
    if (((int32_t)packet.param2 & MAV_DO_REPOSITION_FLAGS_CHANGE_MODE) ||
        (plane.control_mode == &plane.mode_guided)) {
        plane.set_mode(plane.mode_guided, ModeReason::GCS_COMMAND);

        // add home alt if needed
        if (requested_position.relative_alt) {
            requested_position.alt += plane.home.alt;
            requested_position.relative_alt = 0;
        }

        plane.set_guided_WP(requested_position);

        // Loiter radius for planes. Positive radius in meters, direction is controlled by Yaw (param4) value, parsed above
        if (!isnan(packet.param3) && packet.param3 > 0) {
            plane.mode_guided.set_radius_and_direction(packet.param3, requested_position.loiter_ccw);
        }

        return MAV_RESULT_ACCEPTED;
    }
    return MAV_RESULT_FAILED;
}

// these are GUIDED mode commands that are RATE or slew enabled, so you can have more powerful control than default controls.
MAV_RESULT GCS_MAVLINK_Plane::handle_command_int_guided_slew_commands(const mavlink_command_int_t &packet)
{
  switch(packet.command) {
    
#if OFFBOARD_GUIDED == ENABLED
    case MAV_CMD_GUIDED_CHANGE_SPEED: {
        // command is only valid in guided mode
        if (plane.control_mode != &plane.mode_guided) {
            return MAV_RESULT_FAILED;
        }

         // only airspeed commands are supported right now...
        if (int(packet.param1) != SPEED_TYPE_AIRSPEED) {  // since SPEED_TYPE is int in range 0-1 and packet.param1 is a *float* this works.
            return MAV_RESULT_DENIED;
        }

         // reject airspeeds that are outside of the tuning envelope
        if (packet.param2 > plane.aparm.airspeed_max || packet.param2 < plane.aparm.airspeed_min) {
            return MAV_RESULT_DENIED;
        }

         // no need to process any new packet/s with the
         //  same airspeed any further, if we are already doing it.
        float new_target_airspeed_cm = packet.param2 * 100;
        if ( is_equal(new_target_airspeed_cm,plane.guided_state.target_airspeed_cm)) { 
            return MAV_RESULT_ACCEPTED;
        }
        plane.guided_state.target_airspeed_cm = new_target_airspeed_cm;
        plane.guided_state.target_airspeed_time_ms = AP_HAL::millis();

         if (is_zero(packet.param3)) {
            // the user wanted /maximum acceleration, pick a large value as close enough
            plane.guided_state.target_airspeed_accel = 1000.0f;
        } else {
            plane.guided_state.target_airspeed_accel = fabsf(packet.param3);
        }

         // assign an acceleration direction
        if (plane.guided_state.target_airspeed_cm < plane.target_airspeed_cm) {
            plane.guided_state.target_airspeed_accel *= -1.0f;
        }
        return MAV_RESULT_ACCEPTED;
    }

     case MAV_CMD_GUIDED_CHANGE_ALTITUDE: {
        // command is only valid in guided
        if (plane.control_mode != &plane.mode_guided) {
            return MAV_RESULT_FAILED;
        }

        // disallow default value of -1 and dangerous value of zero
        if (is_equal(packet.z, -1.0f) || is_equal(packet.z, 0.0f)){
            return MAV_RESULT_DENIED;
        }

         // the requested alt data might be relative or absolute
        float new_target_alt = packet.z * 100;
        float new_target_alt_rel = packet.z * 100 + plane.home.alt;

         // only global/relative/terrain frames are supported
        switch(packet.frame) {
            case MAV_FRAME_GLOBAL_RELATIVE_ALT: {
                if   (is_equal(plane.guided_state.target_alt,new_target_alt_rel) ) { // compare two floats as near-enough
                    // no need to process any new packet/s with the same ALT any further, if we are already doing it.
                    return MAV_RESULT_ACCEPTED;
                }
                plane.guided_state.target_alt = new_target_alt_rel;
                break;
            }
            case MAV_FRAME_GLOBAL: {
                if   (is_equal(plane.guided_state.target_alt,new_target_alt) ) {  // compare two floats as near-enough
                    // no need to process any new packet/s with the same ALT any further, if we are already doing it.
                    return MAV_RESULT_ACCEPTED;
                }
                plane.guided_state.target_alt = new_target_alt;
                break;
            }
            default:
                //  MAV_RESULT_DENIED  means Command is invalid (is supported but has invalid parameters).
                return MAV_RESULT_DENIED;
        }

        plane.guided_state.target_alt_frame = packet.frame;
        plane.guided_state.last_target_alt = plane.current_loc.alt; // FIXME: Reference frame is not corrected for here
        plane.guided_state.target_alt_time_ms = AP_HAL::millis();

        if (is_zero(packet.param3)) {
            // the user wanted /maximum acceleration, pick a large value as close enough
            plane.guided_state.target_alt_accel = 1000.0;
        } else {
            plane.guided_state.target_alt_accel = fabsf(packet.param3);
        }

         // assign an acceleration direction
        if (plane.guided_state.target_alt < plane.current_loc.alt) {
            plane.guided_state.target_alt_accel *= -1.0f;
        }
        return MAV_RESULT_ACCEPTED;
    }

     case MAV_CMD_GUIDED_CHANGE_HEADING: {

        // command is only valid in guided mode
        if (plane.control_mode != &plane.mode_guided) {
            return MAV_RESULT_FAILED;
        }

         // don't accept packets outside of [0-360] degree range
        if (packet.param2 < 0.0f || packet.param2 >= 360.0f) {
            return MAV_RESULT_DENIED;
        }

        float new_target_heading = radians(wrap_180(packet.param2));

        // if packet is requesting us to go to the heading we are already going to, we-re already on it.
        if ( (is_equal(new_target_heading,plane.guided_state.target_heading))) { // compare two floats as near-enough
            return MAV_RESULT_ACCEPTED;
        }

        // course over ground
        if ( int(packet.param1) == HEADING_TYPE_COURSE_OVER_GROUND) { // compare as nearest int
            plane.guided_state.target_heading_type = GUIDED_HEADING_COG;
            plane.prev_WP_loc = plane.current_loc;
        // normal vehicle heading
        } else if (int(packet.param1) == HEADING_TYPE_HEADING) { // compare as nearest int
            plane.guided_state.target_heading_type = GUIDED_HEADING_HEADING;
        } else {
            //  MAV_RESULT_DENIED  means Command is invalid (is supported but has invalid parameters).
            return MAV_RESULT_DENIED;
        }

        plane.g2.guidedHeading.reset_I();

        plane.guided_state.target_heading = new_target_heading;
        plane.guided_state.target_heading_accel_limit = MAX(packet.param3, 0.05f);
        plane.guided_state.target_heading_time_ms = AP_HAL::millis();
        return MAV_RESULT_ACCEPTED;
    }
#endif // OFFBOARD_GUIDED == ENABLED


  }
  // anything else ...
  return MAV_RESULT_UNSUPPORTED;

}

MAV_RESULT GCS_MAVLINK_Plane::handle_command_int_packet(const mavlink_command_int_t &packet)
{
    switch(packet.command) {

    case MAV_CMD_DO_REPOSITION:
        return handle_command_int_do_reposition(packet);

    // special 'slew-enabled' guided commands here... for speed,alt, and direction commands
    case MAV_CMD_GUIDED_CHANGE_SPEED:
    case MAV_CMD_GUIDED_CHANGE_ALTITUDE:
    case MAV_CMD_GUIDED_CHANGE_HEADING:
        return handle_command_int_guided_slew_commands(packet);

    case MAV_CMD_DO_FOLLOW:
#if AP_SCRIPTING_ENABLED
        // param1: sysid of target to follow
        if ((packet.param1 > 0) && (packet.param1 <= 255)) {
            plane.g2.follow.set_target_sysid((uint8_t)packet.param1);
            return MAV_RESULT_ACCEPTED;
        }
#endif
        return MAV_RESULT_FAILED;
        
    default:
        return GCS_MAVLINK::handle_command_int_packet(packet);
    }
}

MAV_RESULT GCS_MAVLINK_Plane::handle_command_long_packet(const mavlink_command_long_t &packet)
{
    switch(packet.command) {

    case MAV_CMD_DO_CHANGE_SPEED: {
        // if we're in failsafe modes (e.g., RTL, LOITER) or in pilot
        // controlled modes (e.g., MANUAL, TRAINING)
        // this command should be ignored since it comes in from GCS
        // or a companion computer:
        if ((!plane.control_mode->is_guided_mode()) &&
            (plane.control_mode != &plane.mode_auto)) {
            // failed
            return MAV_RESULT_FAILED;
        }

        AP_Mission::Mission_Command cmd;
        if (AP_Mission::mavlink_cmd_long_to_mission_cmd(packet, cmd) != MAV_MISSION_ACCEPTED) {
            return MAV_RESULT_DENIED;
        }
        if (plane.do_change_speed(cmd)) {
            return MAV_RESULT_ACCEPTED;
        }
        return MAV_RESULT_FAILED;
    }

    case MAV_CMD_NAV_LOITER_UNLIM:
        plane.set_mode(plane.mode_loiter, ModeReason::GCS_COMMAND);
        return MAV_RESULT_ACCEPTED;

    case MAV_CMD_NAV_RETURN_TO_LAUNCH:
        plane.set_mode(plane.mode_rtl, ModeReason::GCS_COMMAND);
        return MAV_RESULT_ACCEPTED;

#if HAL_QUADPLANE_ENABLED
    case MAV_CMD_NAV_TAKEOFF: {
        // user takeoff only works with quadplane code for now
        // param7 : altitude [metres]
        float takeoff_alt = packet.param7;
        if (plane.quadplane.available() && plane.quadplane.do_user_takeoff(takeoff_alt)) {
            return MAV_RESULT_ACCEPTED;
        }
        return MAV_RESULT_FAILED;
    }
#endif  // HAL_QUADPLANE_ENABLED

    case MAV_CMD_MISSION_START:
        plane.set_mode(plane.mode_auto, ModeReason::GCS_COMMAND);
        return MAV_RESULT_ACCEPTED;

    case MAV_CMD_DO_LAND_START:
        // attempt to switch to next DO_LAND_START command in the mission
        if (plane.mission.jump_to_landing_sequence()) {
            plane.set_mode(plane.mode_auto, ModeReason::GCS_COMMAND);
            return MAV_RESULT_ACCEPTED;
        }
        return MAV_RESULT_FAILED;

    case MAV_CMD_DO_GO_AROUND:
        {
            uint16_t mission_id = plane.mission.get_current_nav_cmd().id;
            bool is_in_landing = (plane.flight_stage == AP_FixedWing::FlightStage::LAND) ||
                                 (mission_id == MAV_CMD_NAV_LAND) ||
                                 (mission_id == MAV_CMD_NAV_VTOL_LAND);
            if (is_in_landing) {
                // fly a user planned abort pattern if available
                if (plane.mission.jump_to_abort_landing_sequence()) {
                    return MAV_RESULT_ACCEPTED;
                }

                // only fly a fixed wing abort if we aren't doing quadplane stuff, or potentially
                // shooting a quadplane approach
#if HAL_QUADPLANE_ENABLED
                const bool attempt_go_around =
                    (!plane.quadplane.available()) ||
                    ((!plane.quadplane.in_vtol_auto()) &&
                     (!plane.quadplane.landing_with_fixed_wing_spiral_approach()));
#else
                const bool attempt_go_around = true;
#endif
                if (attempt_go_around) {
                    // Initiate an aborted landing. This will trigger a pitch-up and
                    // climb-out to a safe altitude holding heading then one of the
                    // following actions will occur, check for in this order:
                    // - If MAV_CMD_CONTINUE_AND_CHANGE_ALT is next command in mission,
                    //      increment mission index to execute it
                    // - else if DO_LAND_START is available, jump to it
                    // - else decrement the mission index to repeat the landing approach

                    if (!is_zero(packet.param1)) {
                        plane.auto_state.takeoff_altitude_rel_cm = packet.param1 * 100;
                    }
                    if (plane.landing.request_go_around()) {
                        plane.auto_state.next_wp_crosstrack = false;
                        return MAV_RESULT_ACCEPTED;
                    }
                }
            }
        }
        return MAV_RESULT_FAILED;

    case MAV_CMD_DO_SET_HOME: {
        // param1 : use current (1=use current location, 0=use specified location)
        // param5 : latitude
        // param6 : longitude
        // param7 : altitude (absolute)
        if (is_equal(packet.param1,1.0f)) {
            if (!plane.set_home_persistently(AP::gps().location())) {
                return MAV_RESULT_FAILED;
            }
            AP::ahrs().lock_home();
        } else {
            // ensure param1 is zero
            if (!is_zero(packet.param1)) {
                return MAV_RESULT_FAILED;
            }
            Location new_home_loc;
            if (!location_from_command_t(packet, MAV_FRAME_GLOBAL, new_home_loc)) {
                return MAV_RESULT_DENIED;
            }
            if (!set_home(new_home_loc, true)) {
                return MAV_RESULT_FAILED;
            }
        }
        if ((plane.control_mode == &plane.mode_rtl)
#if HAL_QUADPLANE_ENABLED
                || (plane.control_mode == &plane.mode_qrtl)
#endif
                                                            ) {
            // if in RTL head to the updated home location
            plane.control_mode->enter();
        }
        return MAV_RESULT_ACCEPTED;
    }

    case MAV_CMD_DO_AUTOTUNE_ENABLE:
        // param1 : enable/disable
        plane.autotune_enable(!is_zero(packet.param1));
        return MAV_RESULT_ACCEPTED;

#if PARACHUTE == ENABLED
    case MAV_CMD_DO_PARACHUTE:
        // configure or release parachute
        switch ((uint16_t)packet.param1) {
        case PARACHUTE_DISABLE:
            plane.parachute.enabled(false);
            return MAV_RESULT_ACCEPTED;
        case PARACHUTE_ENABLE:
            plane.parachute.enabled(true);
            return MAV_RESULT_ACCEPTED;
        case PARACHUTE_RELEASE:
            // treat as a manual release which performs some additional check of altitude
            if (plane.parachute.released()) {
                gcs().send_text(MAV_SEVERITY_NOTICE, "Parachute already released");
                return MAV_RESULT_FAILED;
            }
            if (!plane.parachute.enabled()) {
                gcs().send_text(MAV_SEVERITY_NOTICE, "Parachute not enabled");
                return MAV_RESULT_FAILED;
            }
            if (!plane.parachute_manual_release()) {
                return MAV_RESULT_FAILED;
            }
            return MAV_RESULT_ACCEPTED;
        default:
            break;
        }
        return MAV_RESULT_FAILED;
#endif

#if HAL_QUADPLANE_ENABLED
    case MAV_CMD_DO_MOTOR_TEST:
        // param1 : motor sequence number (a number from 1 to max number of motors on the vehicle)
        // param2 : throttle type (0=throttle percentage, 1=PWM, 2=pilot throttle channel pass-through. See MOTOR_TEST_THROTTLE_TYPE enum)
        // param3 : throttle (range depends upon param2)
        // param4 : timeout (in seconds)
        // param5 : motor count (number of motors to test in sequence)
        return plane.quadplane.mavlink_motor_test_start(chan,
                                                        (uint8_t)packet.param1,
                                                        (uint8_t)packet.param2,
                                                        (uint16_t)packet.param3,
                                                        packet.param4,
                                                        (uint8_t)packet.param5);

    case MAV_CMD_DO_VTOL_TRANSITION:
        if (!plane.quadplane.handle_do_vtol_transition((enum MAV_VTOL_STATE)packet.param1)) {
            return MAV_RESULT_FAILED;
        }
        return MAV_RESULT_ACCEPTED;
#endif

#if AP_ICENGINE_ENABLED
    case MAV_CMD_DO_ENGINE_CONTROL:
        if (!plane.g2.ice_control.engine_control(packet.param1, packet.param2, packet.param3)) {
            return MAV_RESULT_FAILED;
        }
        return MAV_RESULT_ACCEPTED;
#endif

#if AP_SCRIPTING_ENABLED
    case MAV_CMD_DO_FOLLOW:
        // param1: sysid of target to follow
        if ((packet.param1 > 0) && (packet.param1 <= 255)) {
            plane.g2.follow.set_target_sysid((uint8_t)packet.param1);
            return MAV_RESULT_ACCEPTED;
        }
        return MAV_RESULT_FAILED;
#endif
        
    default:
        return GCS_MAVLINK::handle_command_long_packet(packet);
    }
}

// this is called on receipt of a MANUAL_CONTROL packet and is
// expected to call manual_override to override RC input on desired
// axes.
void GCS_MAVLINK_Plane::handle_manual_control_axes(const mavlink_manual_control_t &packet, const uint32_t tnow)
{
    manual_override(plane.channel_roll, packet.y, 1000, 2000, tnow);
    manual_override(plane.channel_pitch, packet.x, 1000, 2000, tnow, true);
    manual_override(plane.channel_throttle, packet.z, 0, 1000, tnow);
    manual_override(plane.channel_rudder, packet.r, 1000, 2000, tnow);
}

void GCS_MAVLINK_Plane::handleMessage(const mavlink_message_t &msg)
{
    switch (msg.msgid) {

    case MAVLINK_MSG_ID_RADIO:
    case MAVLINK_MSG_ID_RADIO_STATUS:
    {
        handle_radio_status(msg, plane.should_log(MASK_LOG_PM));
        break;
    }

    case MAVLINK_MSG_ID_TERRAIN_DATA:
    case MAVLINK_MSG_ID_TERRAIN_CHECK:
#if AP_TERRAIN_AVAILABLE
        plane.terrain.handle_data(chan, msg);
#endif
        break;

    case MAVLINK_MSG_ID_SET_ATTITUDE_TARGET:
    {
        // Only allow companion computer (or other external controller) to
        // control attitude in GUIDED mode.  We DON'T want external control
        // in e.g., RTL, CICLE. Specifying a single mode for companion
        // computer control is more safe (even more so when using
        // FENCE_ACTION = 4 for geofence failures).
        if (plane.control_mode != &plane.mode_guided) { // don't screw up failsafes
            break; 
        }

        mavlink_set_attitude_target_t att_target;
        mavlink_msg_set_attitude_target_decode(&msg, &att_target);

        // Mappings: If any of these bits are set, the corresponding input should be ignored.
        // NOTE, when parsing the bits we invert them for easier interpretation but transport has them inverted
        // bit 1: body roll rate
        // bit 2: body pitch rate
        // bit 3: body yaw rate
        // bit 4: unknown
        // bit 5: unknown
        // bit 6: reserved
        // bit 7: throttle
        // bit 8: attitude

        // if not setting all Quaternion values, use _rate flags to indicate which fields.

        // Extract the Euler roll angle from the Quaternion.
        Quaternion q(att_target.q[0], att_target.q[1],
                att_target.q[2], att_target.q[3]);

        // NOTE: att_target.type_mask is inverted for easier interpretation
        att_target.type_mask = att_target.type_mask ^ 0xFF;

        uint8_t attitude_mask = att_target.type_mask & 0b10000111; // q plus rpy

        uint32_t now = AP_HAL::millis();
        if ((attitude_mask & 0b10000001) ||    // partial, including roll
                (attitude_mask == 0b10000000)) { // all angles
            plane.guided_state.forced_rpy_cd.x = degrees(q.get_euler_roll()) * 100.0f;

            // Update timer for external roll to the nav control
            plane.guided_state.last_forced_rpy_ms.x = now;
        }

        if ((attitude_mask & 0b10000010) ||    // partial, including pitch
                (attitude_mask == 0b10000000)) { // all angles
            plane.guided_state.forced_rpy_cd.y = degrees(q.get_euler_pitch()) * 100.0f;

            // Update timer for external pitch to the nav control
            plane.guided_state.last_forced_rpy_ms.y = now;
        }

        if ((attitude_mask & 0b10000100) ||    // partial, including yaw
                (attitude_mask == 0b10000000)) { // all angles
            plane.guided_state.forced_rpy_cd.z = degrees(q.get_euler_yaw()) * 100.0f;

            // Update timer for external yaw to the nav control
            plane.guided_state.last_forced_rpy_ms.z = now;
        }
        if (att_target.type_mask & 0b01000000) { // throttle
            plane.guided_state.forced_throttle = att_target.thrust * 100.0f;

            // Update timer for external throttle
            plane.guided_state.last_forced_throttle_ms = now;
        }

        break;
    }

    case MAVLINK_MSG_ID_SET_POSITION_TARGET_LOCAL_NED:
    {
        // decode packet
        mavlink_set_position_target_local_ned_t packet;
        mavlink_msg_set_position_target_local_ned_decode(&msg, &packet);

        // exit if vehicle is not in Guided mode
        if (plane.control_mode != &plane.mode_guided) {
            break;
        }

        // only local moves for now
        if (packet.coordinate_frame != MAV_FRAME_LOCAL_OFFSET_NED) {
            break;
        }

        // just do altitude for now
        plane.next_WP_loc.alt += -packet.z*100.0;
        gcs().send_text(MAV_SEVERITY_INFO, "Change alt to %.1f",
                        (double)((plane.next_WP_loc.alt - plane.home.alt)*0.01));
        
        break;
    }

    case MAVLINK_MSG_ID_SET_POSITION_TARGET_GLOBAL_INT:
    {
        // Only want to allow companion computer position control when
        // in a certain mode to avoid inadvertently sending these
        // kinds of commands when the autopilot is responding to problems
        // in modes such as RTL, CIRCLE, etc.  Specifying ONLY one mode
        // for companion computer control is more safe (provided
        // one uses the FENCE_ACTION = 4 (RTL) for geofence failures).
        if (plane.control_mode != &plane.mode_guided) {
            //don't screw up failsafes
            break;
        }

        mavlink_set_position_target_global_int_t pos_target;
        mavlink_msg_set_position_target_global_int_decode(&msg, &pos_target);
        // Unexpectedly, the mask is expecting "ones" for dimensions that should
        // be IGNORNED rather than INCLUDED.  See mavlink documentation of the
        // SET_POSITION_TARGET_GLOBAL_INT message, type_mask field.
        const uint16_t alt_mask = 0b1111111111111011; // (z mask at bit 3)
            
        bool msg_valid = true;
        AP_Mission::Mission_Command cmd = {0};
        
        if (pos_target.type_mask & alt_mask)
        {
            cmd.content.location.alt = pos_target.alt * 100;
            cmd.content.location.relative_alt = false;
            cmd.content.location.terrain_alt = false;
            switch (pos_target.coordinate_frame) 
            {
                case MAV_FRAME_GLOBAL:
                case MAV_FRAME_GLOBAL_INT:
                    break; //default to MSL altitude
                case MAV_FRAME_GLOBAL_RELATIVE_ALT_INT:
                    cmd.content.location.relative_alt = true;
                    break;
                case MAV_FRAME_GLOBAL_TERRAIN_ALT_INT:
                    cmd.content.location.relative_alt = true;
                    cmd.content.location.terrain_alt = true;
                    break;
                default:
                    gcs().send_text(MAV_SEVERITY_WARNING, "Invalid coord frame in SET_POSTION_TARGET_GLOBAL_INT");
                    msg_valid = false;
                    break;
            }    

            if (msg_valid) {
                handle_change_alt_request(cmd);
            }
        } // end if alt_mask       

        break;
    }

    default:
        handle_common_message(msg);
        break;
    } // end switch
} // end handle mavlink

MAV_RESULT GCS_MAVLINK_Plane::handle_command_do_set_mission_current(const mavlink_command_long_t &packet)
{
    const MAV_RESULT result = GCS_MAVLINK::handle_command_do_set_mission_current(packet);
    if (result != MAV_RESULT_ACCEPTED) {
        return result;
    }

    // if you change this you must change handle_mission_set_current
    plane.auto_state.next_wp_crosstrack = false;
    if (plane.control_mode == &plane.mode_auto && plane.mission.state() == AP_Mission::MISSION_STOPPED) {
        plane.mission.resume();
    }

    return result;
}

void GCS_MAVLINK_Plane::handle_mission_set_current(AP_Mission &mission, const mavlink_message_t &msg)
{
    // if you change this you must change handle_command_do_set_mission_current
    plane.auto_state.next_wp_crosstrack = false;
    GCS_MAVLINK::handle_mission_set_current(mission, msg);
    if (plane.control_mode == &plane.mode_auto && plane.mission.state() == AP_Mission::MISSION_STOPPED) {
        plane.mission.resume();
    }
}

uint64_t GCS_MAVLINK_Plane::capabilities() const
{
    return (MAV_PROTOCOL_CAPABILITY_MISSION_FLOAT |
            MAV_PROTOCOL_CAPABILITY_COMMAND_INT |
            MAV_PROTOCOL_CAPABILITY_MISSION_INT |
            MAV_PROTOCOL_CAPABILITY_SET_POSITION_TARGET_GLOBAL_INT |
            MAV_PROTOCOL_CAPABILITY_SET_ATTITUDE_TARGET |
#if AP_TERRAIN_AVAILABLE
            (plane.terrain.enabled() ? MAV_PROTOCOL_CAPABILITY_TERRAIN : 0) |
#endif
            GCS_MAVLINK::capabilities());
}

#if HAL_HIGH_LATENCY2_ENABLED
int16_t GCS_MAVLINK_Plane::high_latency_target_altitude() const
{
    AP_AHRS &ahrs = AP::ahrs();
    struct Location global_position_current;
    UNUSED_RESULT(ahrs.get_location(global_position_current));

#if HAL_QUADPLANE_ENABLED
    const QuadPlane &quadplane = plane.quadplane;
    //return units are m
    if (quadplane.show_vtol_view()) {
        return (plane.control_mode != &plane.mode_qstabilize) ? 0.01 * (global_position_current.alt + quadplane.pos_control->get_pos_error_z_cm()) : 0;
    }
#endif
    return 0.01 * (global_position_current.alt + plane.altitude_error_cm);
}

uint8_t GCS_MAVLINK_Plane::high_latency_tgt_heading() const
{
    // return units are deg/2
#if HAL_QUADPLANE_ENABLED
    const QuadPlane &quadplane = plane.quadplane;
    if (quadplane.show_vtol_view()) {
        const Vector3f &targets = quadplane.attitude_control->get_att_target_euler_cd();
        return ((uint16_t)(targets.z * 0.01)) / 2;
    }
#endif
        const AP_Navigation *nav_controller = plane.nav_controller;
        // need to convert -18000->18000 to 0->360/2
        return wrap_360_cd(nav_controller->target_bearing_cd() ) / 200;
}

// return units are dm
uint16_t GCS_MAVLINK_Plane::high_latency_tgt_dist() const
{
#if HAL_QUADPLANE_ENABLED
    const QuadPlane &quadplane = plane.quadplane;
    if (quadplane.show_vtol_view()) {
        bool wp_nav_valid = quadplane.using_wp_nav();
        return (wp_nav_valid ? MIN(quadplane.wp_nav->get_wp_distance_to_destination(), UINT16_MAX) : 0) / 10;
    }
    #endif

    return MIN(plane.auto_state.wp_distance, UINT16_MAX) / 10;
}

uint8_t GCS_MAVLINK_Plane::high_latency_tgt_airspeed() const
{
    // return units are m/s*5
    return plane.target_airspeed_cm * 0.05;
}

uint8_t GCS_MAVLINK_Plane::high_latency_wind_speed() const
{
    Vector3f wind;
    wind = AP::ahrs().wind_estimate();

    // return units are m/s*5
    return MIN(wind.length() * 5, UINT8_MAX);
}

uint8_t GCS_MAVLINK_Plane::high_latency_wind_direction() const
{
    const Vector3f wind = AP::ahrs().wind_estimate();

    // return units are deg/2
    // need to convert -180->180 to 0->360/2
    return wrap_360(degrees(atan2f(-wind.y, -wind.x))) / 2;
}
#endif // HAL_HIGH_LATENCY2_ENABLED

MAV_VTOL_STATE GCS_MAVLINK_Plane::vtol_state() const
{
#if !HAL_QUADPLANE_ENABLED
    return MAV_VTOL_STATE_UNDEFINED;
#else
    if (!plane.quadplane.available()) {
        return MAV_VTOL_STATE_UNDEFINED;
    }

    return plane.quadplane.transition->get_mav_vtol_state();
#endif
};

MAV_LANDED_STATE GCS_MAVLINK_Plane::landed_state() const
{
    if (plane.is_flying()) {
        // note that Q-modes almost always consider themselves as flying
        return MAV_LANDED_STATE_IN_AIR;
    }

    return MAV_LANDED_STATE_ON_GROUND;
}