Hidden-mode fault-tolerant spacecraft attitude estimation and control

Aviran Sadon; Daniel Choukroun

Hidden-mode fault-tolerant spacecraft attitude estimation and control

Department of Mechanical Engineering

Research output: Contribution to conference › Paper › peer-review

Abstract

This paper is concerned with a novel design approach for suboptimal control and estimation of a class of Markovian jump linear systems with hidden mode and partial state information. The efficiency of the proposed approach is illustrated via comparative results of an extensive Monte-Carlo simulation for a simple system. Furthermore, the application to fault-tolerant spacecraft attitude estimation and control is suggested.

Original language	English
State	Published - 1 Jan 2016
Event	56th Israel Annual Conference on Aerospace Sciences, IACAS 2016 - Tel-Aviv and Haifa, Israel Duration: 9 Mar 2016 → 10 Mar 2016

Conference

Conference	56th Israel Annual Conference on Aerospace Sciences, IACAS 2016
Country/Territory	Israel
City	Tel-Aviv and Haifa
Period	9/03/16 → 10/03/16

ASJC Scopus subject areas

Space and Planetary Science
Aerospace Engineering

Cite this

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AB - This paper is concerned with a novel design approach for suboptimal control and estimation of a class of Markovian jump linear systems with hidden mode and partial state information. The efficiency of the proposed approach is illustrated via comparative results of an extensive Monte-Carlo simulation for a simple system. Furthermore, the application to fault-tolerant spacecraft attitude estimation and control is suggested.

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T2 - 56th Israel Annual Conference on Aerospace Sciences, IACAS 2016

Y2 - 9 March 2016 through 10 March 2016

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Hidden-mode fault-tolerant spacecraft attitude estimation and control

Abstract

Conference

ASJC Scopus subject areas

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