On a class of nonlinear optimal synchronization and tracking control problems

In this paper, we consider a new class of nonlinear optimal tracking and synchronization control problems subject to control constraints, where the motions of two distinct objects are required to achieve synchronization at the minimum time while achieving the optimal tracking of a reference target....

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Main Authors: Zhou, Jingyang, Teo, Kok Lay
Format: Journal Article
Published: Kyushu Tokai University 2011
Online Access:http://www.ijicic.org/ijicic-10-01043.pdf
http://hdl.handle.net/20.500.11937/42668
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author Zhou, Jingyang
Teo, Kok Lay
author_facet Zhou, Jingyang
Teo, Kok Lay
author_sort Zhou, Jingyang
building Curtin Institutional Repository
collection Online Access
description In this paper, we consider a new class of nonlinear optimal tracking and synchronization control problems subject to control constraints, where the motions of two distinct objects are required to achieve synchronization at the minimum time while achieving the optimal tracking of a reference target. A computational method is developed for constructing such an optimal switching control law. The method proposed is then used to solve a practical problem, which arises from the study of the angular velocity tracking and synchronization of two spacecrafts during their formation flight. The results obtained are highly satisfactory.
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format Journal Article
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institution Curtin University Malaysia
institution_category Local University
last_indexed 2025-11-14T09:12:56Z
publishDate 2011
publisher Kyushu Tokai University
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spelling curtin-20.500.11937-426682017-01-30T15:01:20Z On a class of nonlinear optimal synchronization and tracking control problems Zhou, Jingyang Teo, Kok Lay In this paper, we consider a new class of nonlinear optimal tracking and synchronization control problems subject to control constraints, where the motions of two distinct objects are required to achieve synchronization at the minimum time while achieving the optimal tracking of a reference target. A computational method is developed for constructing such an optimal switching control law. The method proposed is then used to solve a practical problem, which arises from the study of the angular velocity tracking and synchronization of two spacecrafts during their formation flight. The results obtained are highly satisfactory. 2011 Journal Article http://hdl.handle.net/20.500.11937/42668 http://www.ijicic.org/ijicic-10-01043.pdf Kyushu Tokai University restricted
spellingShingle Zhou, Jingyang
Teo, Kok Lay
On a class of nonlinear optimal synchronization and tracking control problems
title On a class of nonlinear optimal synchronization and tracking control problems
title_full On a class of nonlinear optimal synchronization and tracking control problems
title_fullStr On a class of nonlinear optimal synchronization and tracking control problems
title_full_unstemmed On a class of nonlinear optimal synchronization and tracking control problems
title_short On a class of nonlinear optimal synchronization and tracking control problems
title_sort on a class of nonlinear optimal synchronization and tracking control problems
url http://www.ijicic.org/ijicic-10-01043.pdf
http://hdl.handle.net/20.500.11937/42668