Attitude control of microsatellite

176 p.

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Main Author: Luo, Wencheng
Other Authors: Chu Yun Chung
Format: Theses and Dissertations
Published: 2011
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Online Access:https://hdl.handle.net/10356/46907
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Institution: Nanyang Technological University
id sg-ntu-dr.10356-46907
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spelling sg-ntu-dr.10356-469072023-07-04T16:58:26Z Attitude control of microsatellite Luo, Wencheng Chu Yun Chung School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering 176 p. In this thesis, we study the robust optimal attitude control problem of microsatellites with disturbances and an uncertain inertia matrix. This is a nonlinear control problem. As the emphasis is on the development of state-feedback attitude controllers that achieve optimality as well as disturbance attenuation, a brief survey is made of the Lyapunov stability and the disturbance attenuation problems of nonlinear systems. DOCTOR OF PHILOSOPHY (EEE) 2011-12-27T05:43:55Z 2011-12-27T05:43:55Z 2005 2005 Thesis Luo, W. (2005). Attitude control of microsatellite. Doctoral thesis, Nanyang Technological University, Singapore. https://hdl.handle.net/10356/46907 10.32657/10356/46907 Nanyang Technological University application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
topic DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
spellingShingle DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
Luo, Wencheng
Attitude control of microsatellite
description 176 p.
author2 Chu Yun Chung
author_facet Chu Yun Chung
Luo, Wencheng
format Theses and Dissertations
author Luo, Wencheng
author_sort Luo, Wencheng
title Attitude control of microsatellite
title_short Attitude control of microsatellite
title_full Attitude control of microsatellite
title_fullStr Attitude control of microsatellite
title_full_unstemmed Attitude control of microsatellite
title_sort attitude control of microsatellite
publishDate 2011
url https://hdl.handle.net/10356/46907
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