能量收集
航天器
振动
控制理论(社会学)
隔振
能量(信号处理)
四边形的
参数统计
刚度
工程类
计算机科学
声学
物理
航空航天工程
数学
结构工程
统计
控制(管理)
量子力学
人工智能
有限元法
作者
Shitong Fang,Keyu Chen,Zhihui Lai,Shengxi Zhou,Daniil Yurchenko,Wei-Hsin Liao
标识
DOI:10.1016/j.ymssp.2023.110466
摘要
Vibrations and drifting motions of a post-capture spacecraft may lead to its instability and safety risk, which therefore need to be absorbed or isolated. However, it is expected that the vibrational energy is not wasted but harvested to power the wireless sensors. Motivated by this concept and inspired by the movement of a bird, a quadrilateral shape isolation system with an energy harvester is proposed for the simultaneous broadband vibration isolation and energy harvesting of the post-capture spacecraft. The governing equations of the proposed system are derived based on Hamilton’s principle. The corresponding dimensionless approximate analytical model is deduced based on the harmonic balance method and validated through the comparison with the numerical Runge–Kutta method. Simulation results demonstrate that compared with its counterpart without the energy harvester, the proposed system can further improve the broadband vibration isolation performance, and achieve the energy harvesting function simultaneously. The operation principle is the energy localization effect, which is demonstrated through the investigation on system dynamics. The guideline for improving the dual performances is proposed according to the parametric studies on the mass ratios, the equivalent stiffness and damping induced by the quadrilateral shape structures, and the mechanical and electrical parameters of the energy harvester.
科研通智能强力驱动
Strongly Powered by AbleSci AI