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

AN EXPERIMENT RESEARCH ON TECHNIQUE OF ATTITUDE DETERMINATION WITH DOUBLE SATELLITES

doi: 10.11728/cjss2000.03.257
  • Received Date: 1999-11-08
  • Rev Recd Date: 2000-05-10
  • Publish Date: 2000-08-24
  • 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.

     

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