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

向前变椭圆

Tsinghua University Press, Beijing and Springer-Verlag Berlin Heidelberg 2013

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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

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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

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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

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