首页> 外国专利> Aircraft airflow sensor with error correction based on aircraft movement and calibration process of said sensor based on aircraft movement

Aircraft airflow sensor with error correction based on aircraft movement and calibration process of said sensor based on aircraft movement

机译:基于飞机运动误差修正的飞机气流传感器及基于飞机运动的传感器校准过程

摘要

An aircraft airflow sensor probe comprising: a vane assembly configured to sense a direction of local airflow external to the aircraft; a shaft configured to rotatably hold the vane assembly and permit rotational movement of the vane assembly; at least one accelerometer configured to detect aircraft movement; a sensor for detecting and outputting a rotational position of the vane assembly; an angle of attack processor configured to determine at least a measured angle of attack of the aircraft based on a rotational position of the vane assembly; The at least one accelerometer is configured to provide aircraft motion data to the angle of attack processor. and the angle of attack processor is further configured to determine a calibration value based on aircraft motion data provided by the at least one accelerometer and output a calibrated angle of attack of the aircraft.
机译:一种飞机气流传感器探头,包括:叶片组件,其被配置为感测飞机外部的局部气流方向;轴,其被配置成可旋转地保持所述叶片组件并允许所述叶片组件旋转运动;至少一个加速计,用于检测飞机的运动;传感器,用于检测和输出叶片组件的旋转位置;迎角处理器,其被配置为基于所述叶片组件的旋转位置来确定所述飞机的至少测量的迎角;至少一个加速计被配置为向迎角处理器提供飞机运动数据。攻角处理器进一步配置为基于由至少一个加速计提供的飞机运动数据确定校准值,并输出飞机的校准攻角。

著录项

  • 公开/公告号KR20220046703A

    专利类型

  • 公开/公告日2022-04-14

    原文格式PDF

  • 申请/专利权人 에어로소닉 엘엘씨;

    申请/专利号KR1020227010640

  • 发明设计人 스나이더 릭;랭 찰스;

    申请日2020-08-31

  • 分类号G01P21/02;B64F5/60;G01C23;G01P13/02;G01P15;G01P5/14;

  • 国家 KR

  • 入库时间 2022-08-25 00:38:18

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号