Control Allocation for Spacecraft Under Actuator Faults

Qinglei Hu; Bo Li; Bing Xiao; Youmin Zhang

doi:10.1007/978-981-16-0439-3

Control Allocation for Spacecraft Under Actuator Faults

Qinglei Hu, Bo Li, Bing Xiao, Youmin Zhang

School of Automation

Research output: Book/Report › Book › peer-review

16 Scopus citations

Abstract

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.

Original language	English
Publisher	Springer Singapore
Number of pages	221
ISBN (Electronic)	9789811604393
ISBN (Print)	9789811604386
DOIs	https://doi.org/10.1007/978-981-16-0439-3
State	Published - 1 Jan 2021

Keywords

Actuator Failures
Attitude Control
Control Allocation
Fault Tolerant Control
Finite-Time Control
Spacecraft

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10.1007/978-981-16-0439-3

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abstract = "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.",

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AB - 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.

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KW - Attitude Control

KW - Control Allocation

KW - Fault Tolerant Control

KW - Finite-Time Control

KW - Spacecraft

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Control Allocation for Spacecraft Under Actuator Faults

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