Control allocation for spacecraft under actuator faults / Qinglei Hu, Bo Li, Bing Xiao, Youmin Zhang.
Hu, Qinglei, author.; Li, Bo, editor.; Xiao, Bing, editor.; Zhang, Youmin, 1965- editor.
2021
TL3260 .H8 2021eb
Available Online

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Title Control allocation for spacecraft under actuator faults / Qinglei Hu, Bo Li, Bing Xiao, Youmin Zhang.
Author Hu, Qinglei, author.
ISBN 9789811604393 (electronic bk.)
9811604398 (electronic bk.)
9789811604386
981160438X
DOI https://doi.org/10.1007/978-981-16-0439-3
Published Singapore : Springer, [2021]
Copyright ©2021
Language English
Description 1 online resource (xviii, 221 pages)
Other Standard Identifiers 10.1007/978-981-16-0439-3 doi
Call Number TL3260 .H8 2021eb
Dewey Decimal Classification 629.47/42
Summary This book provides a systematical and comprehensive description of some facets of modeling, designing, analyzing and exploring the control allocation and fault-tolerant control problems for over-actuated spacecraft attitude control system under actuator failures, system uncertainties and disturbances. The book intends to provide a unified platform for understanding and applicability of the fault-tolerant attitude control and control allocation for different purposes in aerospace engineering and some related fields. And it is particularly suited for readers who are interested to learn solutions in spacecraft attitude control system design and related engineering applications.
Bibliography, etc. Note Includes bibliographical references.
Access Note Access limited to authorized users.
Source of Description Description based on print version record.
Added Author Li, Bo, editor.
Xiao, Bing, editor.
Zhang, Youmin, 1965- editor.
Available in Other Form Control Allocation for Spacecraft under Actuator Faults.
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Record Appears in Online Resources > Ebooks
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Introduction
Mathematical Model of the Attitude Control System
Null-Space Based Optimal Control Allocation for Spacecraft Attitude Stabilization
Robust Finite-Time Control Allocation for Attitude Stabilization Under Actuator Misalignment
Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation
Extended State Observer Based Optimal Attitude Robust Control of Spacecraft
Spacecraft Attitude Fault-Tolerant Control Based on Iterative Learning Observer and Control Allocation
Nonlinear Proportional-Derivative Control Incorporating Closed-Loop Control Allocation for Spacecraft
Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults
Conclusions.

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