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一类刚-梁耦合系统平面稳态运动的稳定性 被引量:2

PLANAR MOTION AND STABILITY FOR A RIGID BODY ATTACHED WITH A FLEXIBLE ATTACHMENT IN A FIELD OF CENTRAL GRAVITATIONAL FORCE
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摘要 研究了中心力场中的一类刚-弹耦合系统的平面运动动力学,模型是带有一悬臂梁的刚体.综合考虑了系统轨道运动与姿态运动,在Lagrange力学体系下给出了系统的运动方程,在保守系统和考虑梁的材料黏滞阻尼两种情况下,利用能量-动量方法给出了一类相对平衡点稳定性的充分条件. Planar motion for a rigid body attached with an elastic beam in a field of central gravitational force was investigated, and both of orbital motion and attitude motion were under consideration. The equations of motion of the system were derived by Lagrangian equation. The system has a first integral which indicates the conservation of angular momentum of the system. In the case of conservative system, the system has a class of relative equilibria which correspond to stationary motions of the system. Each stationary motion is defined by steady rotation of the system at an angular velocity equal to the orbital velocity, with the beam being in deformed state. By taking the energy-momentum functional as the Lyapunov function, the sufficient conditions for the stability of the relative equilibria were given. In the case of the energy dissipation, if the dissipation comes from the material viscous-damping of the beam, such energy dissipation do not change the relative equilibria of the sysstem, so the sufficient conditions for the stability of the stationary motions are the same.
作者 程耀 陆启韶
出处 《力学学报》 EI CSCD 北大核心 2005年第6期750-755,共6页 Chinese Journal of Theoretical and Applied Mechanics
基金 国家自然科学基金资助项目(19402005).~~
关键词 中心力场 刚-弹耦合 相对平衡点 稳定性 能量-动量方法 central gravitational force, coupled rigid-elastic body, relative equilibrium, stability, EnergyMomentum method
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参考文献9

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同被引文献27

  • 1洪嘉振,尤超蓝.刚柔耦合系统动力学研究进展[J].动力学与控制学报,2004,2(2):1-6. 被引量:40
  • 2刘锦阳,李彬,洪嘉振.作大范围空间运动柔性梁的刚-柔耦合动力学[J].力学学报,2006,38(2):276-282. 被引量:22
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  • 5Chaikin SV. Equilibria stability of the satellite as a system with a countable number of degrees of freedom. Acta Astronautica, 2001, 48(4): 193-202.
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  • 10Dong WN, Schlack AL Jr. Stability of a spinning satellite with flexible antennas. AIAA Journal, 1974, 12(12): 1737-1739.

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