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Flight Vehicle Attitude Determination Using the Modified Rodrigues Parameters
There are two attitude estimation algorithms based on the different representations of attitude errors when modified Rodrigues parameters are applied to attitude estimation. The first is multiplicative error attitude estimator (MEAE), whose attitude error is expressed by the modified Rodrigues parameters representing the rotation from the estimated to the true attitude. The second is subtractive error attitude estimator (SEAE), whose attitude error is expressed by the arithmetic difference between the true and the estimated attitudes. It is proved that the two algorithms are equivalent in the case of small attitude errors. It is possible to describe rotation without encountering singularity by switching between the modified Rodrigues parameters and their shadow parameters. The attitude parameter switching does not bring disturbance to MEAE, but it does to SEAE. This article introduces a modification to eliminate the disturbance on SEAE,and simulation results demonstrate the efficacy of the presented algorithm.
作 者： Chen Jizheng Yuan Jianping Fang Qun 作者單位： College of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China 刊 名： 中國(guó)航空學(xué)報(bào)(英文版) ISTIC 英文刊名： CHINESE JOURNAL OF AERONAUTICS 年，卷(期)： 2008 21(5) 分類號(hào)： V2 關(guān)鍵詞： attitude estimation modified Rodrigues parameters singularity attitude error【Flight Vehicle Attitude Determinatio】相關(guān)文章：
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