向前变椭圆 发表于 2025-3-25 05:45:55
Tsinghua University Press, Beijing and Springer-Verlag Berlin Heidelberg 2013addition 发表于 2025-3-25 08:42:43
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’sCalibrate 发表于 2025-3-25 11:58:14
http://reply.papertrans.cn/23/2239/223881/223881_23.png刺激 发表于 2025-3-25 17:00:30
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讥讽 发表于 2025-3-25 20:53:17
http://reply.papertrans.cn/23/2239/223881/223881_25.pngCOM 发表于 2025-3-26 03:30:35
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淡紫色花 发表于 2025-3-26 06:16:28
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http://image.papertrans.cn/c/image/223881.jpgNarrative 发表于 2025-3-26 14:43:46
9楼Medicaid 发表于 2025-3-26 18:27:54
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