國立高雄大學圖資館 |

Language: English

Back

Control allocation for spacecraft un...

Hu, Qinglei.

Control allocation for spacecraft under actuator faults

Record Type:	Electronic resources : Monograph/item
Title/Author:	Control allocation for spacecraft under actuator faultsby Qinglei Hu ... [et al.].
other author:	Hu, Qinglei.
Published:	Singapore :Springer Singapore :2021.
Description:	xviii, 221 p. :ill., digital ;24 cm.
Contained By:	Springer Nature eBook
Subject:	Space vehiclesAttitude control systems.
Online resource:	https://doi.org/10.1007/978-981-16-0439-3
ISBN:	9789811604393$q(electronic bk.)

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$q(electronic bk.)

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

681475
Space vehicles
--Attitude control systems.

LC Class. No.: TL3260

Dewey Class. No.: 629.4742

Control allocation for spacecraft under actuator faults
LDR:02379nmm a2200337 a 4500 001 599593
003 DE-He213
005 20210713113555.0
006 m d
007 cr nn 008maaau
008 211027s2021 si s 0 eng d
020 $a 9789811604393$q(electronic bk.)
020 $a 9789811604386$q(paper)
024 7 $a 10.1007/978-981-16-0439-3 $2 doi
035 $a 978-981-16-0439-3
040 $a GP $c GP
041 0 $a eng
050 4 $a TL3260
072 7 $a TJFM $2 bicssc
072 7 $a TEC004000 $2 bisacsh
072 7 $a TJFM $2 thema
072 7 $a TJFD $2 thema
082 0 4 $a 629.4742 $2 23
090 $a TL3260 $b .C764 2021
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 Space vehicles $x Attitude control systems. $3 681475
650 0 $a Actuators. $3 224320
650 1 4 $a Control, Robotics, Mechatronics. $3 339147
650 2 4 $a Aerospace Technology and Astronautics. $3 309707
700 1 $a Hu, Qinglei. $3 893805
710 2 $a SpringerLink (Online service) $3 273601
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)