Fault detection and recovery of spacecraft formation flying using nonlinear observer and reconfigurable controller

Daren Lee; Krishna Dev Kumar; Manoranjan Sinha

doi:10.1016/j.actaastro.2013.12.002

Fault detection and recovery of spacecraft formation flying using nonlinear observer and reconfigurable controller

Authors

Lee, Daren
Kumar, Krishna Dev
Sinha, Manoranjan^{1, 2, 1, 3}

¹ Department of Aerospace Engineering
² Ryerson University
³ Indian Institute of Technology Kharagpur

Type

Published Article

Journal

Acta Astronautica

Publisher

Elsevier

Publication Date

Jan 01, 2014

Accepted Date

Dec 04, 2013

Volume

Pages

58–72

Identifiers

DOI: 10.1016/j.actaastro.2013.12.002

Source

Elsevier

Keywords

Spacecraft Formation Flying
Nonlinear Observer
Reconfigurable Controller
Fault Reconstruction And Recovery
Sliding Mode Technique

License

Unknown

Abstract

Highlights•A novel scheme for fault detection and recovery of spacecraft formations.•The proposed scheme is based on a state observer and a reconfigurable controller.•The state observer is designed based on the super twisting sliding mode technique•The reconfigurable controller is developed using the sliding mode technique.•Theoretical proofs along with simulation results validate the proposed scheme.

Abstract

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