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Titlebook: Chaos in Attitude Dynamics of Spacecraft; Yanzhu Liu,Liqun Chen Book 2013 Tsinghua University Press, Beijing and Springer-Verlag Berlin He

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发表于 2025-3-21 18:04:28 | 显示全部楼层 |阅读模式
书目名称Chaos in Attitude Dynamics of Spacecraft
编辑Yanzhu Liu,Liqun Chen
视频videohttp://file.papertrans.cn/224/223881/223881.mp4
概述Contains necessary knowledge on chaos and its control in spacecraft attitude dynamics.Summarizes the research work of Chinese scientists in this field
图书封面Titlebook: Chaos in Attitude Dynamics of Spacecraft; Yanzhu Liu,Liqun Chen Book 2013 Tsinghua University Press, Beijing and Springer-Verlag Berlin He
描述.Attitude dynamics is the theoretical basis of attitude control of spacecrafts in aerospace engineering. With the development of nonlinear dynamics, chaos in spacecraft attitude dynamics has drawn great attention since the 1990‘s. The problem of the predictability and controllability of the chaotic attitude motion of a spacecraft has a practical significance in astronautic science. This book aims to summarize basic concepts, main approaches, and recent progress in this area. It focuses on the research work of the author and other Chinese scientists in this field, providing new methods and viewpoints in the investigation of spacecraft attitude motion, as well as new mathematical models, with definite engineering backgrounds, for further analysis..Professor Yanzhu Liu was the Director of the Institute of Engineering Mechanics, Shanghai Jiao Tong University, China. Dr. Liqun Chen is a Professor at the Department of Mechanics, Shanghai University, China..
出版日期Book 2013
关键词TUP; aerospace; astronautics; mechanics; spacecraft
版次1
doihttps://doi.org/10.1007/978-3-642-30080-6
isbn_ebook978-3-642-30080-6
copyrightTsinghua University Press, Beijing and Springer-Verlag Berlin Heidelberg 2013
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Chaos in Spatial Attitude Motion of Spacecraft,ret-Andoyer variables, which are introduced to simplify the dynamical models. The influences of the gravitational and magnetic fields on the attitude motion are revisited using the new variables. A rigid body in elliptic orbit and gravitational field, a torque-free rigid body with eccentrically rota
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Control of Chaotic Attitude Motion,stem theory. The OGY method is presented as a significant and representative approach. Synchronization of chaos is briefly introduced. The parametric open-plus-closed-loop method and the stability criterion method are respectively proposed with the main ideas, the control laws, and the numerical exa
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https://doi.org/10.1007/978-3-642-41556-2ular orbit under gravitational torque are analyzed by using the first approximation method and the Lyapunov’s direct method. The attitude motions of a gyrostat are analyzed as a model of spacecraft with axisymmetric rotors. The permanent rotations and its stability of a spinning spacecraft are discussed under torque-free assumption.
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https://doi.org/10.1007/978-3-642-41556-2ction of gravitational and magnetic field of the Earth. The numerical results not only confirm the existence of chaotic motion, but also serve as examples of geometrical structure of chaos, routes to chaos, and numerical identification of chaos.
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Primer on Spacecraft Dynamics,ular orbit under gravitational torque are analyzed by using the first approximation method and the Lyapunov’s direct method. The attitude motions of a gyrostat are analyzed as a model of spacecraft with axisymmetric rotors. The permanent rotations and its stability of a spinning spacecraft are discussed under torque-free assumption.
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