A discrete-time observer design for spacecraft attitude determination using an orthogonality preserving algorithm
A discrete-time observer design for spacecraft attitude determination using an orthogonality preserving algorithm
This paper studies a nonlinear discrete-time partial state observer design problem for rigid spacecraft systems, particularly for spacecraft attitude estimation. The construction is inspired by an orthogonalitypreserving numerical algorithm, and it yields a semiglobal practical asymptotic observer. We show that the separation principle holds, and hence stabilization using output feedback is possible. An example is provided to illustrate the usefulness of our results in a sampled-data implementation of an attitude control for a rigid spacecraft using output feedback and to illustrate the advantages of the proposed observer design, especially compared to a sample and hold version of a similar type observer designed in continuous-time.
spacecraft systems, discrete-time observer, nonlinear sampled-data systems, orthogonality preservation, asymptotic stabilization, output feedback
975-980
Laila, Dina Shona
41aa5cf9-3ec2-4fdf-970d-a0a349bfd90c
Lovera, Marco
4387af7a-7b24-4ad5-84c2-69d10c263794
Astolfi, Alessandro
3045f9a9-e8f3-4f19-9f5d-08364de75cdb
May 2011
Laila, Dina Shona
41aa5cf9-3ec2-4fdf-970d-a0a349bfd90c
Lovera, Marco
4387af7a-7b24-4ad5-84c2-69d10c263794
Astolfi, Alessandro
3045f9a9-e8f3-4f19-9f5d-08364de75cdb
Laila, Dina Shona, Lovera, Marco and Astolfi, Alessandro
(2011)
A discrete-time observer design for spacecraft attitude determination using an orthogonality preserving algorithm.
Automatica, 47 (5), .
(doi:10.1016/j.automatica.2011.01.049).
Abstract
This paper studies a nonlinear discrete-time partial state observer design problem for rigid spacecraft systems, particularly for spacecraft attitude estimation. The construction is inspired by an orthogonalitypreserving numerical algorithm, and it yields a semiglobal practical asymptotic observer. We show that the separation principle holds, and hence stabilization using output feedback is possible. An example is provided to illustrate the usefulness of our results in a sampled-data implementation of an attitude control for a rigid spacecraft using output feedback and to illustrate the advantages of the proposed observer design, especially compared to a sample and hold version of a similar type observer designed in continuous-time.
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Published date: May 2011
Keywords:
spacecraft systems, discrete-time observer, nonlinear sampled-data systems, orthogonality preservation, asymptotic stabilization, output feedback
Organisations:
Mechatronics
Identifiers
Local EPrints ID: 199505
URI: http://eprints.soton.ac.uk/id/eprint/199505
ISSN: 0005-1098
PURE UUID: 7c01425b-1e66-4e24-a501-3fe7b7a500e1
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Date deposited: 18 Oct 2011 13:11
Last modified: 14 Mar 2024 04:16
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Contributors
Author:
Dina Shona Laila
Author:
Marco Lovera
Author:
Alessandro Astolfi
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