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A two-stage extended kalman filter method for fault estimation of satellite attitude control systems

  • Published:2017-01 Issue:2 Volume:354 Page:872-886
  • ISSN:0016-0032
  • Container-title:Journal of the Franklin Institute
  • language:en
  • Short-container-title:Journal of the Franklin Institute

Author:

Chen Xueqin,Liu Ming

Funder

New Century Excellent Talents Program of the Ministry of Education of China

the National Natural Science Foundation of China

Open Fund of National Defense Key Discipline Laboratory of Micro-Spacecraft Technology

Publisher

Elsevier BV

Subject

Applied Mathematics,Computer Networks and Communications,Signal Processing,Control and Systems Engineering

Reference37 articles.

1. Fault detection and fault-tolerant control of a civil aircraft using a sliding-mode-based scheme;Alwi;IEEE Trans. Control Syst.Technol.,2008

2. Research on improved integrated FDD/FTC with effectiveness factors;Chen;J. Syst. Eng. Electron.,2012

3. Application of effectiveness factors to integrated FDD and FTC of satellite attitude control systems;Chen;Acta Astronautica,2009

4. Event-triggered robust distributed state estimation for sensor networks with state-dependent noises;Dong;Int. J. General Syst.,2015

5. Finite-horizon estimation of randomly occurring faults for a class of nonlinear time-varying systems;Dong;Automatica,2014

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