中国科技核心期刊

中文核心期刊

CSCD来源期刊

空间控制技术与应用 ›› 2023, Vol. 49 ›› Issue (3): 85-96.doi: 10.3969/j.issn.1674 1579.2023.03.010

• 论文与报告 • 上一篇    

轨道平面外直线形绳系编队系统运动状态解析关系

  

  1. 南京航空航天大学航空航天结构力学及控制国家重点实验室
  • 出版日期:2023-06-26 发布日期:2023-07-17
  • 基金资助:
    国家自然科学基金资助项目(12072147)、江苏省自然科学基金(BK20211177)和航空科学基金(2020Z063052001)

Analytical Relationship of Motion States of a Linear Tethered Formation in ontypical Planes

  • Online:2023-06-26 Published:2023-07-17

摘要: 本文研究正交控制力约束下,轨道平面外三星直线排列的绳系编队系统动力学特性.在非惯性坐标系下构建系统动力学模型,其中卫星和两根起连接作用系绳分别简化为质点和无质量弹簧,推导系统状态与系统动力学的解析关系式及对运动形式间临界状态的影响.提出一个三维动力学参数域以展示系统在任意轨道面内动力学,并通过数值仿真进行验证,结果显示解析计算结果与仿真结果完全一致.

关键词: 直线形编队, 轨道平面外, 参数域, 临界状态, 解析关系

Abstract: The dynamics of a linear tethered system with three satellites in nontypical plane with orthogonal control force is studied in this paper. An approximate but useful model for a high dimensional nonlinear system is established in the non inertial frame, where three satellites and two space tethers are deemed to be particles and massless springs, respectively. The analytical relationship between the initial state and dynamics and its influence on the critical state of dynamic behavior are derived. A three dimensional dynamic parameter domain is proposed to demonstrate the dynamics in any orbital plane, and verified by numerical simulation. The results show that the analytical calculation is completely consistent with the simulation.

Key words: linear tethered formation, nontypical plane, critical state, analytical relationship

中图分类号: 

  • O322