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Titlebook: Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters; Jie Wang,Dong-Xu Li Book 2022 The Editor

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书目名称Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters
编辑Jie Wang,Dong-Xu Li
视频video
概述Is the first book available on control theories for systems in complex mode space.Includes detailed formulation of multi-body dynamics and control theories.Involves massive simulation results to help
图书封面Titlebook: Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters;  Jie Wang,Dong-Xu Li Book 2022 The Editor
描述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..
出版日期Book 2022
关键词Flexible spacecraft with time-varying parameters; Coupling control; Complex mode; Active vibration cont
版次1
doihttps://doi.org/10.1007/978-981-16-5097-0
isbn_softcover978-981-16-5099-4
isbn_ebook978-981-16-5097-0
copyrightThe Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapor
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发表于 2025-3-21 23:24:12 | 显示全部楼层
ontrol theories.Involves massive simulation results to help 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 st
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978-981-16-5099-4The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapor
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Rigid-Flexible Coupling Dynamic Analysis of Flexible Spacecraft,The main purpose of this chapter is to calculate the dynamic characteristics of the flexible spacecraft with time-varying parameters based on the model in the previous chapter, and to obtain the dynamic responses of the spacecraft under typical cases
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