國立高雄大學圖資館 |

Language: English

Back

Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters

Record Type:	Electronic resources : Monograph/item
Title/Author:	Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parametersby Jie Wang, Dong-Xu Li.
Author:	Wang, Jie.
other author:	Li, Dong-Xu.
Published:	Singapore :Springer Singapore :2022.
Description:	ix, 185 p. :ill. (some col.), digital ;24 cm.
Contained By:	Springer Nature eBook
Subject:	Space vehiclesAttitude control systems.
Online resource:	https://doi.org/10.1007/978-981-16-5097-0
ISBN:	9789811650970$q(electronic bk.)

Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters
Wang, Jie.

Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters[electronic resource] /by Jie Wang, Dong-Xu Li. - Singapore :Springer Singapore :2022. - ix, 185 p. :ill. (some col.), digital ;24 cm.

Introduction -- Modeling of Flexible Spacecraft with Time-varying Parameters -- Dynamic Analysis of Flexible Spacecraft with Time-varying Parameters -- Vibration Control Methods for Systems in Complex Mode Space -- Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft -- Coupling Control Method for Flexible Spacecraft -- Attitude Coupling Control Experiments -- Future.

This book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable amplitudes input shaping methods and coupling control methods are proposed for stabilization of flexible spacecraft. The research provides an important way to solve the problem of high-precision attitude control of flexible spacecraft with time-varying parameters. This book is appropriate for the researchers who focus on the multi-body dynamics, attitude and vibration control of flexible spacecraft.

ISBN: 9789811650970$q(electronic bk.)

Standard No.: 10.1007/978-981-16-5097-0doiSubjects--Topical Terms:

681475
Space vehicles
--Attitude control systems.

LC Class. No.: TL3260 / .W36 2022

Dewey Class. No.: 629.4742

Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters
LDR:02344nmm a2200325 a 4500 001 618160
003 DE-He213
005 20210915075101.0
006 m d
007 cr nn 008maaau
008 221025s2022 si s 0 eng d
020 $a 9789811650970$q(electronic bk.)
020 $a 9789811650963$q(paper)
024 7 $a 10.1007/978-981-16-5097-0 $2 doi
035 $a 978-981-16-5097-0
040 $a GP $c GP
041 0 $a eng
050 4 $a TL3260 $b .W36 2022
072 7 $a TJFM $2 bicssc
072 7 $a TEC004000 $2 bisacsh
072 7 $a TJFM $2 thema
082 0 4 $a 629.4742 $2 23
090 $a TL3260 $b .W246 2022
100 1 $a Wang, Jie. $3 227117
245 1 0 $a Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters $h [electronic resource] / $c by Jie Wang, Dong-Xu Li.
260 $a Singapore : $b Springer Singapore : $b Imprint: Springer, $c 2022.
300 $a ix, 185 p. : $b ill. (some col.), digital ; $c 24 cm.
505 0 $a Introduction -- Modeling of Flexible Spacecraft with Time-varying Parameters -- Dynamic Analysis of Flexible Spacecraft with Time-varying Parameters -- Vibration Control Methods for Systems in Complex Mode Space -- Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft -- Coupling Control Method for Flexible Spacecraft -- Attitude Coupling Control Experiments -- Future.
520 $a This book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable amplitudes input shaping methods and coupling control methods are proposed for stabilization of flexible spacecraft. The research provides an important way to solve the problem of high-precision attitude control of flexible spacecraft with time-varying parameters. This book is appropriate for the researchers who focus on the multi-body dynamics, attitude and vibration control of flexible spacecraft.
650 0 $a Space vehicles $x Attitude control systems. $3 681475
650 0 $a Stability of space vehicles. $3 376163
650 1 4 $a Control and Systems Theory. $3 825946
650 2 4 $a Complexity. $3 274400
650 2 4 $a Aerospace Technology and Astronautics. $3 309707
700 1 $a Li, Dong-Xu. $3 917756
710 2 $a SpringerLink (Online service) $3 273601
773 0 $t Springer Nature eBook
856 4 0 $u https://doi.org/10.1007/978-981-16-5097-0
950 $a Intelligent Technologies and Robotics (SpringerNature-42732)