Application of discrete time sliding mode control to a spacecraft in 6DoF
Application of discrete time sliding mode control to a spacecraft in 6DoF
This paper presents the application of two separate discrete time sliding mode controllers, developed in conjunction with a potential function guidance method, to provide control in both position and attitude for a rigid, holonomic spacecraft body. The system is demonstrated in MATLABTM simulations to illustrate effectiveness
under realistic actuator constraints.
1-10
Lincoln, Nicholas K.
d8bb25d1-2c79-4904-9727-b6cf844334a6
Veres, Sandor M.
909c60a0-56a3-4eb6-83e4-d52742ecd304
Lincoln, Nicholas K.
d8bb25d1-2c79-4904-9727-b6cf844334a6
Veres, Sandor M.
909c60a0-56a3-4eb6-83e4-d52742ecd304
Lincoln, Nicholas K. and Veres, Sandor M.
(2010)
Application of discrete time sliding mode control to a spacecraft in 6DoF.
International Journal of Control, 83 (9), .
(In Press)
Abstract
This paper presents the application of two separate discrete time sliding mode controllers, developed in conjunction with a potential function guidance method, to provide control in both position and attitude for a rigid, holonomic spacecraft body. The system is demonstrated in MATLABTM simulations to illustrate effectiveness
under realistic actuator constraints.
Text
PracticalSMC.pdf
- Author's Original
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Accepted/In Press date: 30 April 2010
Identifiers
Local EPrints ID: 149685
URI: http://eprints.soton.ac.uk/id/eprint/149685
ISSN: 0020-3270
PURE UUID: 5b5c77b1-9fd5-4bce-ab26-8dd7da31e837
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Date deposited: 05 May 2010 07:43
Last modified: 14 Mar 2024 01:11
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Author:
Nicholas K. Lincoln
Author:
Sandor M. Veres
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