標(biāo)題: Titlebook: Chaos in Attitude Dynamics of Spacecraft; Yanzhu Liu,Liqun Chen Book 2013 Tsinghua University Press, Beijing and Springer-Verlag Berlin He [打印本頁] 作者: 空格 時間: 2025-3-21 18:04
書目名稱Chaos in Attitude Dynamics of Spacecraft影響因子(影響力)
書目名稱Chaos in Attitude Dynamics of Spacecraft影響因子(影響力)學(xué)科排名
書目名稱Chaos in Attitude Dynamics of Spacecraft網(wǎng)絡(luò)公開度
書目名稱Chaos in Attitude Dynamics of Spacecraft網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Chaos in Attitude Dynamics of Spacecraft被引頻次
書目名稱Chaos in Attitude Dynamics of Spacecraft被引頻次學(xué)科排名
書目名稱Chaos in Attitude Dynamics of Spacecraft年度引用
書目名稱Chaos in Attitude Dynamics of Spacecraft年度引用學(xué)科排名
書目名稱Chaos in Attitude Dynamics of Spacecraft讀者反饋
書目名稱Chaos in Attitude Dynamics of Spacecraft讀者反饋學(xué)科排名
作者: 劇本 時間: 2025-3-21 20:42 作者: 笨拙的你 時間: 2025-3-22 03:27 作者: 干涉 時間: 2025-3-22 07:19
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作者: 到婚嫁年齡 時間: 2025-3-22 12:04
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作者: FIG 時間: 2025-3-22 14:59
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.作者: FIG 時間: 2025-3-22 20:47
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.作者: Paradox 時間: 2025-3-23 01:12 作者: 糾纏,纏繞 時間: 2025-3-23 04:08 作者: crease 時間: 2025-3-23 05:48
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.作者: anatomical 時間: 2025-3-23 10:00 作者: 織物 時間: 2025-3-23 14:57 作者: 丑惡 時間: 2025-3-23 21:34
Control of Chaotic Attitude Motion,raft in an elliptic orbit in the gravitational and the magnetic field is treated as an example to demonstrate the applications of the parametric open-plus-closed-loop method and the stability criterion method.作者: Orgasm 時間: 2025-3-23 22:54 作者: Visual-Acuity 時間: 2025-3-24 03:56 作者: antenna 時間: 2025-3-24 10:05 作者: intercede 時間: 2025-3-24 14:22 作者: ALT 時間: 2025-3-24 18:51
Book 2013haos 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 作者: gain631 時間: 2025-3-24 19:08
rther 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..978-3-642-30080-6作者: monochromatic 時間: 2025-3-25 03:01
https://doi.org/10.1007/978-3-642-30080-6TUP; aerospace; astronautics; mechanics; spacecraft作者: 向前變橢圓 時間: 2025-3-25 05:45
Tsinghua University Press, Beijing and Springer-Verlag Berlin Heidelberg 2013作者: addition 時間: 2025-3-25 08:42
https://doi.org/10.1007/978-3-642-41556-2a simplified model of orbit motion of a spacecraft around the Earth. The main environmental torques acting on spacecraft, the gravitational torque and magnetic torque are introduced. The dynamical equations of attitude motion of a spacecraft are established, where the Euler’s equations and Poisson’s作者: Calibrate 時間: 2025-3-25 11:58 作者: 刺激 時間: 2025-3-25 17:00
https://doi.org/10.1007/978-3-642-41556-2l and damping torque is discussed, and the Melnikov’s theory is applied to predict the transverse heteroclinic point. The numerical simulations and Poincaré maps are performed to confirm the existence of chaos. The same methods are used to analyze the motion of a tethered satellite in circular orbit作者: 譏諷 時間: 2025-3-25 20:53 作者: COM 時間: 2025-3-26 03:30
https://doi.org/10.1007/978-3-642-41556-2stem 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作者: 淡紫色花 時間: 2025-3-26 06:16 作者: 托運(yùn) 時間: 2025-3-26 10:20
http://image.papertrans.cn/c/image/223881.jpg作者: Narrative 時間: 2025-3-26 14:43
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