Electronics Design of the Airborne Stabilized Platform Attitude Acquisition Module

被引：0

作者：

Xu, Jiang ^{[1
]}

Wei, Guiling ^{[1
]}

Cheng, Yong

Li, Baolin ^{[1
]}

Bu, Hongyi

Wang, Hao ^{[1
]}

Zhang, Zhanwei ^{[1
]}

Li, Xingni

机构：

[1] 26thInst China Elect Technol Grp Corp, Chongqing 400060, Peoples R China

来源：

SELECTED PAPERS FROM CONFERENCES OF THE PHOTOELECTRONIC TECHNOLOGY COMMITTEE OF THE CHINESE SOCIETY OF ASTRONAUTICS: OPTICAL IMAGING, REMOTE SENSING, AND LASER-MATTER INTERACTION 2013 | 2014年 / 9142卷

关键词：

Attitude acquisition; Stabilized platform; Modularization; POS;

D O I：

10.1117/12.2054080

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

We present an attitude acquisition module electronics design for the airborne stabilized platform. The design scheme, which is based on Integrated MEMS sensor ADIS16405, develops the attitude information processing algorithms and the hardware circuit. The hardware circuits with a small volume of only 44.9 x 43.6 x 24.6 mm(3), has the characteristics of lightweight, modularization and digitalization. The interface design of the PC software uses the combination plane chart with track line to receive the attitude information and display. Attitude calculation uses the Kalman filtering algorithm to improve the measurement accuracy of the module in the dynamic environment.

引用

页数：9