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小天体探测器附着缓冲系统设计及稳定性分析

Design and Stability Analysis of Attachment Buffer System for Small Celestial Body Detector

  • 摘要: 面向极弱引力小天体表面附着探测需求,设计了一种三足式探测器附着缓冲系统,开展了附着过程的稳定性分析。为实现在极弱引力环境下无反弹地稳定附着于小天体表面,在考虑着陆速度与倾角误差的前提下,设计了一种二级缓冲系统,分别采用粘扣带剥离耗能和泡沫铝压溃吸能降低接触碰撞过程对探测器稳定性的影响。建立了探测器多体系统动力学模型、探测器足垫−表面碎石接触碰撞动力学模型,基于多体动力学与离散元联合仿真,获得了不同着陆倾角与速度探测器的运动规律。结果表明,二级缓冲系统具有良好的缓冲吸能效果,可有效地防止探测器反弹、滑移和倾覆等现象,在一定倾角与速度范围内探测器能稳定附着于小天体表面。研究成果可为未来小天体探测任务着陆方案设计提供技术支撑。

     

    Abstract: To meet the requirement of adhesion detection on the surface of extremely weak gravitational small celestial bodies, a three-legged detector attachment buffer system was designed, and a stability analysis of the attachment process was carried out. In order to achieve stable attachment to the surface of the small body without rebound in a very weak gravitational environment, a two-stage buffer system was designed considering with the error of landing speed and inclination angle taken into account. The energy consumption of the hook and loop fastener and the crushing energy absorption of the aluminum foam were used to reduce the influence of the contact collision process on the stability of the detector. The multi-body system dynamics model of the detector and the contact collision dynamics model of the detector footpad-granular medium were established. Based on the joint simulation of multi-body dynamics and discrete element, the motion law of the detector under different landing inclination angles and speeds was obtained. The results show that the two-stage buffer system has a good buffer energy absorption effect, which can effectively prevent the detector from rebounding, slipping and overturning. The detector can be stably attached to the surface of the small celestial body within a certain inclination angle and velocity range. The research results can provide technical support for the landing scheme design of small celestial body exploration missions in the future.

     

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