A residual based adaptive unscented Kalman filter for fault recovery in attitude determination system of microsatellites-Reference-Cited by-同舟云学术

A residual based adaptive unscented Kalman filter for fault recovery in attitude determination system of microsatellites

Published:2014-12 Issue:1 Volume:105 Page:30-39
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Le Huy Xuan,Matunaga Saburo

Funder

JSPS

Vietnamese Government

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference14 articles.

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2. Kalman filtering for spacecraft attitude estimation;Lefferts;J. Guid. Control Dyn.,1982

3. Survey of nonlinear attitude estimation methods;Crassidis;AIAA J. Guid. Control Dyn.,2007

4. Unscented filtering for spacecraft attitude estimation;Crassidis;J. Guid. Control Dyn.,2003

5. Model-based Fault Diagnosis Techniques: Design Schemes, Algorithms, and Tools;Ding,2008

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