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Control Allocation for Spacecraft Under Actuator Faults

Record Type:	Language materials, printed : Monograph/item
Title/Author:	Control Allocation for Spacecraft Under Actuator Faults/ by Qinglei Hu, Bo Li, Bing Xiao, Youmin Zhang.
Author:	Hu, Qinglei.
other author:	Li, Bo.
Description:	XVIII, 221 p. 116 illus., 110 illus. in color.online resource. :
Contained By:	Springer Nature eBook
Subject:	Control engineering. -
Online resource:	https://doi.org/10.1007/978-981-16-0439-3
ISBN:	9789811604393

Control Allocation for Spacecraft Under Actuator Faults
Hu, Qinglei.

Control Allocation for Spacecraft Under Actuator Faults[electronic resource] /by Qinglei Hu, Bo Li, Bing Xiao, Youmin Zhang. - 1st ed. 2021. - XVIII, 221 p. 116 illus., 110 illus. in color.online resource.

Introduction -- Spacecraft Model and Control Allocation Formulation -- Null-space based Optimal Control Allocation for Spacecraft Stabilization -- Robust finite-time control allocation under actuator misalignment -- Finite-Time Fault-Tolerant Spacecraft Attitude Control and Control allocation with Torque Saturation -- Fault Tolerant Control Allocation of Spacecraft Using Fault Detection and Diagnosis -- Extended State Observer based Optimal Control Allocation -- Nonlinear Proportional-Derivative Control Incorporating Closed-loop Control Allocation -- Closed-Loop-Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Fault -- Conclusion.

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. .

ISBN: 9789811604393

Standard No.: 10.1007/978-981-16-0439-3doiSubjects--Topical Terms:

1249728
Control engineering.

LC Class. No.: TJ210.2-211.495

Dewey Class. No.: 629.8

Control Allocation for Spacecraft Under Actuator Faults
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505 0 $a Introduction -- Spacecraft Model and Control Allocation Formulation -- Null-space based Optimal Control Allocation for Spacecraft Stabilization -- Robust finite-time control allocation under actuator misalignment -- Finite-Time Fault-Tolerant Spacecraft Attitude Control and Control allocation with Torque Saturation -- Fault Tolerant Control Allocation of Spacecraft Using Fault Detection and Diagnosis -- Extended State Observer based Optimal Control Allocation -- Nonlinear Proportional-Derivative Control Incorporating Closed-loop Control Allocation -- Closed-Loop-Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Fault -- Conclusion.
520 $a 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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