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

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Rigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parametersby Jie Wang, Dong-Xu Li.
作者:	Wang, Jie.
其他作者:	Li, Dong-Xu.
出版者:	Singapore :Springer Singapore :2022.
面頁冊數:	ix, 185 p. :ill. (some col.), digital ;24 cm.
Contained By:	Springer Nature eBook
標題:	Space vehiclesAttitude control systems.
電子資源:	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
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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.
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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.
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650 2 4 $a Aerospace Technology and Astronautics. $3 309707
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