Paper
7 May 2010 Optimize the space combinations of measure-vectors of the integrated star-sensor/gyro systems for spacecrafts
Xiujian Li, Juncai Yang, Jiankun Yang, Hui Jia, Yuanyuan Jiao, Yisheng Yang, Shaofeng Guo, Mengfei Yang, Dayi Wang, Qingchun Fan
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Abstract
In order to achieve continuous attitude information of the spacecrafts or the telescopes, the star-sensors and the gyros are usually integrated to form navigation systems, which measure and determine the attitude-angles synthetically. The space combinations of the measure-vectors of the star-sensors and the gyros are analyzed to find out the influences of the combination modes on the determination precision of the attitude-angles, and the influence trends are summarized. Furthermore, the optimum space combinations of the measure-vectors are proposed for improvement the determination precision of the attitude-angles and the redundancy/complement of star-sensors and gyros. The optimum space combinations of the measure-vectors are benefit for designing optimum integrated star/gyro systems to achieve high determination precision of the attitude-angles, even any of the star-sensors or the gyros works with poor measurement precision, so as to improve the reliability of the navigation systems.
© (2010) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Xiujian Li, Juncai Yang, Jiankun Yang, Hui Jia, Yuanyuan Jiao, Yisheng Yang, Shaofeng Guo, Mengfei Yang, Dayi Wang, and Qingchun Fan "Optimize the space combinations of measure-vectors of the integrated star-sensor/gyro systems for spacecrafts", Proc. SPIE 7691, Space Missions and Technologies, 76910P (7 May 2010); https://doi.org/10.1117/12.850214
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KEYWORDS
Gyroscopes

Space operations

Navigation systems

System integration

Sensors

Optical testing

Space telescopes

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