AN EXPERIMENT RESEARCH ON TECHNIQUE OF ATTITUDE DETERMINATION WITH DOUBLE SATELLITES

ZHENG Wei; WU Jie; HU Xiaoping; ZHAO Jiankang

doi:10.11728/cjss2000.03.257

Volume 20 Issue 3

Aug. 2000

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Article Navigation > Chinese Journal of Space Science > 2000 > 20(3): 257-261

ZHENG Wei, WU Jie, HU Xiaoping, ZHAO Jiankang. AN EXPERIMENT RESEARCH ON TECHNIQUE OF ATTITUDE DETERMINATION WITH DOUBLE SATELLITES[J]. Chinese Journal of Space Science, 2000, 20(3): 257-261. doi: 10.11728/cjss2000.03.257

Citation:

ZHENG Wei, WU Jie, HU Xiaoping, ZHAO Jiankang. AN EXPERIMENT RESEARCH ON TECHNIQUE OF ATTITUDE DETERMINATION WITH DOUBLE SATELLITES[J]. Chinese Journal of Space Science, 2000, 20(3): 257-261. doi: 10.11728/cjss2000.03.257

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AN EXPERIMENT RESEARCH ON TECHNIQUE OF ATTITUDE DETERMINATION WITH DOUBLE SATELLITES

doi: 10.11728/cjss2000.03.257

Department of Aerospace Technology, National University of Defense Technologe, Changsha 410073

Received Date: 1999-11-08
Rev Recd Date: 2000-05-10
Publish Date: 2000-08-24

Abstract

Abstract

The method of attitude determination with double satellites is discussed indetail in the paper, and the actual experiment of attitude determination with onlytwo GPS satellites is conducted. The long-short baseline method and sequenceoptindzation method are synthetically used to estimate carrier phase ambiguity.The experiment results indicate that the success rate of attitude deterndnationexceeds 90% and the mean square error of attitude can be less than 0.5°, whenbaseline length be 1 m around.
- Attitude sensor,
- Satellite navigation,
- Global Positioning System