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Control allocation for spacecraft un...

Hu, Qinglei.

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Control allocation for spacecraft under actuator faults

Record Type:	Electronic resources : Monograph/item
Title/Author:	Control allocation for spacecraft under actuator faults/ by Qinglei Hu ... [et al.].
other author:	Hu, Qinglei.
Published:	Singapore :Springer Singapore : : 2021.,
Description:	xviii, 221 p. :ill., digital ;24 cm.
[NT 15003449]:	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.
Contained By:	Springer Nature eBook
Subject:	Actuators. -
Online resource:	https://doi.org/10.1007/978-981-16-0439-3
ISBN:	9789811604393

Control allocation for spacecraft under actuator faults
Control allocation for spacecraft under actuator faults[electronic resource] /by Qinglei Hu ... [et al.]. - Singapore :Springer Singapore :2021. - xviii, 221 p. :ill., digital ;24 cm.

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:

649246
Actuators.

LC Class. No.: TL3260

Dewey Class. No.: 629.4742

Control allocation for spacecraft under actuator faults
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245 0 0 $a Control allocation for spacecraft under actuator faults $h [electronic resource] / $c by Qinglei Hu ... [et al.].
260 $a Singapore : $b Springer Singapore : $b Imprint: Springer, $c 2021.
300 $a xviii, 221 p. : $b ill., digital ; $c 24 cm.
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.
650 0 $a Actuators. $3 649246
650 0 $a Space vehicles $x Attitude control systems. $3 2068355
650 1 4 $a Control, Robotics, Mechatronics. $3 1002220
650 2 4 $a Aerospace Technology and Astronautics. $3 928116
700 1 $a Hu, Qinglei. $3 3492965
710 2 $a SpringerLink (Online service) $3 836513
773 0 $t Springer Nature eBook
856 4 0 $u https://doi.org/10.1007/978-981-16-0439-3
950 $a Intelligent Technologies and Robotics (SpringerNature-42732)