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Multiple Model Adaptive Rank Estimation for Integrated Navigation during Mars Entry

  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

Accurate navigation systems are required for future pinpoint Mars landing missions. A radio ranging augmented Inertial Measurement Unit (IMU) integrated navigation system concept is considered for the Mars entry navigation. The uncertain system parameters associated with the Three Degree-Of-Freedom (3-DOF) dynamic model, and the measurement systematic errors are considered. In order to improve entry navigation accuracy, this paper presents the Multiple Model Adaptive Rank Estimation (MMARE) filter of radio beacons/IMU integrated navigation system. 3-DOF simulation results show that the performances of the proposed navigation filter method, 70·39 m estimated altitude error and 15·74 m/s estimated velocity error, fulfill the need of future pinpoint Mars landing missions.

源语言英语
页(从-至)291-308
页数18
期刊Journal of Navigation
70
2
DOI
出版状态已出版 - 1 3月 2017

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