首页> 外文会议>第八届国际测试技术研讨会(8th International Symposium on Test and Measurement)论文集 >Wind Measurement Method without Aerodynamics Angles of Attack and Sideslip for Small Unmanned Aircraft Vehicle
【24h】

Wind Measurement Method without Aerodynamics Angles of Attack and Sideslip for Small Unmanned Aircraft Vehicle

机译:小型无人飞行器没有气动动力学迎角和侧滑的测风方法

获取原文
获取外文期刊封面目录资料

摘要

A new approach for on-board determination of the wind speed and direction for small unmanned aircraft vehicle is presented. Using the data from the airspeed system (a nose-mounted pitot tube and temperature sensors) and with the coordinate transformation matrix from the attitude determination system, the air speed vector in the geodetic coordinate system can be obtained by establishing equations. Then, together with the velocity of the aircraft from the aircraft navigation system (GPS), it is possible to estimate the wind vector without angles of attack and sideslip and to achieve the low-cost and convenient goal. Results from simulations are presented for verification of the wind measurement method.
机译:提出了一种用于机载确定小型无人机风速和风向的新方法。使用来自空速系统(机头安装的皮托管和温度传感器)的数据以及姿态确定系统的坐标转换矩阵,可以通过建立方程来获得大地坐标系中的空气速度矢量。然后,与来自飞机导航系统(GPS)的飞机速度一起,可以估计没有迎角和侧滑的风矢量,并实现低成本和便捷的目标。给出了模拟结果,以验证测风方法。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

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