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C++ AP_GPS::horizontal_accuracy方法代码示例

本文整理汇总了C++中AP_GPS::horizontal_accuracy方法的典型用法代码示例。如果您正苦于以下问题:C++ AP_GPS::horizontal_accuracy方法的具体用法?C++ AP_GPS::horizontal_accuracy怎么用?C++ AP_GPS::horizontal_accuracy使用的例子?那么恭喜您, 这里精选的方法代码示例或许可以为您提供帮助。您也可以进一步了解该方法所在AP_GPS的用法示例。


在下文中一共展示了AP_GPS::horizontal_accuracy方法的1个代码示例,这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞,您的评价将有助于系统推荐出更棒的C++代码示例。

示例1: send_dynamic_out

void AP_ADSB::send_dynamic_out(const mavlink_channel_t chan)
{
    // --------------
    // Knowns
    AP_GPS gps = _ahrs.get_gps();
    Vector3f gps_velocity = gps.velocity();

    int32_t latitude = _my_loc.lat;
    int32_t longitude = _my_loc.lng;
    int32_t altGNSS = _my_loc.alt*0.1f; // convert cm to mm
    int16_t velVert = gps_velocity.z * 1E2; // convert m/s to cm/s
    int16_t nsVog = gps_velocity.x * 1E2; // convert m/s to cm/s
    int16_t ewVog = gps_velocity.y * 1E2; // convert m/s to cm/s
    uint8_t fixType = gps.status(); // this lines up perfectly with our enum
    uint8_t emStatus = 0; // TODO: implement this ENUM. no emergency = 0
    uint8_t numSats = gps.num_sats();
    uint16_t squawk = 1200; // Mode A code (typically 1200 [0x04B0] for VFR)

    uint32_t accHoriz = UINT_MAX;
    float accHoriz_f;
    if (gps.horizontal_accuracy(accHoriz_f)) {
        accHoriz = accHoriz_f * 1E3; // convert m to mm
    }

    uint16_t accVert = USHRT_MAX;
    float accVert_f;
    if (gps.vertical_accuracy(accVert_f)) {
        accVert = accVert_f * 1E2; // convert m to cm
    }

    uint16_t accVel = USHRT_MAX;
    float accVel_f;
    if (gps.speed_accuracy(accVel_f)) {
        accVel = accVel_f * 1E3; // convert m/s to mm/s
    }

    uint16_t state = 0;
    if (out_state._is_in_auto_mode) {
        state |= UAVIONIX_ADSB_OUT_DYNAMIC_STATE_AUTOPILOT_ENABLED;
    }
    if (!out_state.is_flying) {
        state |= UAVIONIX_ADSB_OUT_DYNAMIC_STATE_ON_GROUND;
    }



    // --------------
    // Not Sure
    uint32_t utcTime = UINT_MAX; //    uint32_t utcTime,
    // TODO: confirm this sets utcTime correctly
    const uint64_t gps_time = gps.time_epoch_usec();
    utcTime = gps_time / 1000000ULL;



    // --------------
    // Unknowns
    // TODO: implement http://www.srh.noaa.gov/images/epz/wxcalc/pressureAltitude.pdf
    int32_t altPres = INT_MAX; //_ahrs.get_baro().get_altitude() relative to home, not MSL



    mavlink_msg_uavionix_adsb_out_dynamic_send(
            chan,
            utcTime,
            latitude,
            longitude,
            altGNSS,
            fixType,
            numSats,
            altPres,
            accHoriz,
            accVert,
            accVel,
            velVert,
            nsVog,
            ewVog,
            emStatus,
            state,
            squawk);
}
开发者ID:GGPENG,项目名称:ardupilot,代码行数:81,代码来源:AP_ADSB.cpp


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