4.6 Article

Nonlinear filtering for sequential spacecraft attitude estimation with real data: Cubature Kalman Filter, Unscented Kalman Filter and Extended Kalman Filter

期刊

ADVANCES IN SPACE RESEARCH
卷 63, 期 2, 页码 1038-1050

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.asr.2018.10.003

关键词

Attitude estimation; Real data; Euler angles; Cubature Kalman Filter; Extended Kalman Filter; Unscented Kalman Filter

资金

  1. FAPESP (Sao Paulo Research Foundation) [2018/04548-4]
  2. CNPq (Brazilian Council for Scientific and Technological Development) [405468/2016-4, 407296/2016-6, 306790/2014-9]

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This article compares the attitude estimated by nonlinear estimator Cubature Kalman Filter with results obtained by the Extended Kalman Filter and Unscented Kalman Filter. Currently these estimators are the subject of great interest in attitude estimation problems, however, mostly the Extended Kalman Filter has been applied to real problems of this nature. In order to evaluate the behavior of the Extended Kalman Filter, Unscented Kalman Filter and Cubature Kalman Filter algorithms when submitted to realistic situations, this paper uses real data of sensors on-board the CBERS-2 remote sensing satellite (China Brazil Earth Resources Satellite). It is observed that, for the case studied in this article, the filters are very competitive and present advantages and disadvantages that should be dealt with according to the requirements of the problem. (C) 2018 COSPAR. Published by Elsevier Ltd. All rights reserved.

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