21 February 2014 Electronics design of the airborne stabilized platform attitude acquisition module
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Abstract
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 mm3, 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.
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Jiang Xu, Jiang Xu, Guiling Wei, Guiling Wei, Yong Cheng, Yong Cheng, Baolin Li, Baolin Li, Hongyi Bu, Hongyi Bu, Hao Wang, Hao Wang, Zhanwei Zhang, Zhanwei Zhang, Xingni Li, Xingni Li, } "Electronics design of the airborne stabilized platform attitude acquisition module", Proc. SPIE 9142, Selected Papers from Conferences of the Photoelectronic Technology Committee of the Chinese Society of Astronautics: Optical Imaging, Remote Sensing, and Laser-Matter Interaction 2013, 91421E (21 February 2014); doi: 10.1117/12.2054080; https://doi.org/10.1117/12.2054080
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