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超声波阵列的飞行高度与姿态测量方法
引用本文:杨景阳,李荣冰,杭义军,刘建业.超声波阵列的飞行高度与姿态测量方法[J].航空计算技术,2013(5):128-131.
作者姓名:杨景阳  李荣冰  杭义军  刘建业
作者单位:南京航空航天大学导航研究中心,江苏南京210016
基金项目:江苏省研究生培养创新工程项目资助(CXZZ12_0159);江苏省高校优势学科建设工程项目资助
摘    要:针对无人机近地面降落阶段对相对高度及姿态精确测量的需求,以固定翼无人机为对象,设计了多路超声波测距传感器在无人机上的新型布局方式。利用空间几何关系,建立相对高度及姿态计算模型,测得四个固定点的高度,为无人机着陆提供精确的相对高度及姿态角信息。充分利用布置在无人机不同位置的测距传感器之间的几何关系,直接获得姿态角,提高了无人机降落阶段的安全性。实验结果表明,能够及时有效地提供给控制台无人机着陆时的相对高度及姿态信息,准确指引无人机的安全降落。

关 键 词:微惯性姿态角测量系统  超声波定高系统  多路超声波测距传感器  相对高度及姿态

A Measuring Method of Flight Altitude and Attitude Measurement Based on Ultrasonic Array
Institution:YANG Jing- yang, LI Rong- bing, HANG Yi- jun, LIU Jian- ye ( Navigation Research Center, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)
Abstract:In view of the demand for the precise measuement of the relative altitude and attitude angle dur- ing UAV landing on the ground,based on fixed-wing UAV, Multi-channel ranging sensor on UAV's new layout is designed. Using spatial geometrical relations to build model of relative altitude and attitude angle, with the height of four fixed point measured, accurate message of relative altitude and attitude angle is pro- vided for landing UAV. This method take full use of geometrical relation between ultrasonic ranging sensors in different positions on UAV, and get the attitude angle as a result directly, which enhance safety during UAV landing. The test results show that the method can provide the message of relative altitude and attitude angle during UAV landing to console immediately and guide UAV to land safely and accurately.
Keywords:micro inertial attitude angle measurement system  ultrasonic altitude survey  multi- channelultrasonic ranging sensor  relative altitude and attitude angle
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