Study of FOG+Star Sensor Satellites Attitude Determination System

摘要：

During the satellites normal working stage, the accuracy of the attitude measure is very high. The thesis introduces an approach of FOG+star sensor, and designs the kalman filtering algorithm for attitude determination. The result of arith simulation shows that the approach is satisfied the requirements.

关键词： fiber optic gyro(FOG) star sensor Kalman filtering

作者: Huang Wei Wen Guo-yi Chen Jia-bin Zhang Yan-shun

作者单位: The First Aeronautic Institute of Air Force, Xinyang, Henan, China, 464000 Beijing institute of technology, Beijing, China, 100081 Beijing University of Astronautics and Aeronautics, Beijing, China, 100083

会议类型: 国际会议

会议名称: 第八届国际测试技术研讨会(8th International Symposium on Test and Measurement)

会议地点: 重庆

会议语种:英文

页码: 2839-2842

在线出版日期: 2009-08-01（万方平台首次上网日期，不代表论文的发表时间）