光电传感器姿态参考系统的测试方法

A. Szelmanowski, Sławomir Michalak
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引用次数: 0

摘要

本文研究了在圆锥激励/运动作用下姿态参考系统的测试方法。本文对所讨论的励磁进行了理论描述,并对具有倾斜平台的UPG-48站产生的励磁进行了比较分析。对姿态航向参考系统AHRS LCR-92系统非完整激励/运动测试的实验数据,与光电传感器姿态航向参考系统数值模型的仿真测试结果进行了比较。本文根据AutoCAD包中一些数值模拟的结果,提出了美国空军理工学院的圆锥励磁测量站的概念。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The method of testing of the attitude reference systems with optoelectronic sensors
What the paper deals with is the method of testing of the attitude reference systems with the coning excitation/motion applied. A theoretical description of the excitation at issue has been given and followed with a comparative analysis of the excitation generated in the UPG-48 station with a tilting platform. Experimental data of testing of the attitude and heading reference system AHRS LCR-92 system for the non-holonomical excitation/motion have been compared with results effected by some simulation-based tests of numerical models of the attitude and heading reference systems with the optoelectronic sensors. On the grounds of some numerical-simulation-effected findings gained with the AutoCAD packet, a concept of a coning-excitation-generating measuring station has been developed at the Air Force Institute of Technology and presented in this paper.
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