Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters / Jie Wang, Dong-Xu Li.
Wang, Jie, author.; Li, Dong-Xu, author.
2022
TL3260 .W36 2022
Available Online

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Title Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters / Jie Wang, Dong-Xu Li.
Author Wang, Jie, author.
ISBN 9789811650970 (electronic bk.)
9811650977 (electronic bk.)
9789811650963
9811650969
DOI https://doi.org/10.1007/978-981-16-5097-0
Published Singapore : Springer, [2022]
Copyright ©2022
Language English
Description 1 online resource : illustrations (some color)
Other Standard Identifiers 10.1007/978-981-16-5097-0 doi
Call Number TL3260 .W36 2022
Dewey Decimal Classification 629.47/42
Summary 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.
Bibliography, etc. Note Includes bibliographical references.
Access Note Access limited to authorized users.
Digital File Characteristics text file
PDF
Source of Description Online resource; title from PDF title page (SpringerLink, viewed September 23, 2021).
Added Author Li, Dong-Xu, author.
Available in Other Form Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters.
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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.

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