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

空格

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)學科排名




書目名稱Chaos in Attitude Dynamics of Spacecraft網(wǎng)絡公開度




書目名稱Chaos in Attitude Dynamics of Spacecraft網(wǎng)絡公開度學科排名




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讀者反饋學科排名

劇本

笨拙的你

干涉

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

到婚嫁年齡

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

FIG

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.

FIG

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.

Paradox

糾纏,纏繞

crease

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.