大型网架式可展开空间结构的非线性动力学与控制

胡海岩; 田强; 张伟; 金栋平; 胡更开; 宋燕平

doi:10.6052/1000-0992-13-045

大型网架式可展开空间结构的非线性动力学与控制

doi: 10.6052/1000-0992-13-045

1 北京理工大学飞行器动力学与控制教育部重点实验室, 北京100081
2 南京航空航天大学机械结构力学及控制国家重点实验室, 南京200016
3 北京工业大学机电学院, 北京100124
4 中国空间技术研究院西安分院, 西安710100

基金项目: 国家自然科学基金重大资助项目(11290150)

详细信息

作者简介:
胡海岩, 1956年出生, 1988年毕业于南京航空航天大学固体力学专业, 获工学博士. 现任北京理工大学校长、教授, 中国科学院院士, 发展中国家科学院院士；兼任中国科学院技术科学部副主任, 中国力学学会理事长, 中国宇航学会副理事长, 中国航空学会副理事长. 主要从事飞行器结构动力学与控制、非线性动力学与控制等领域的研究, 曾获国家自然科学奖二等奖, 国家科技进步奖二等奖, 何梁何利科学与技术进步奖(数学力学奖).

通讯作者:
胡海岩

中图分类号: O313, O322
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出版历程
- 收稿日期: 2013-06-19
- 修回日期: 2013-07-19
- 刊出日期: 2013-07-25

Nonlinear Dynamics and Control of Large Deployable Space Structures Composed of Trusses and Meshes

1 MOE Key Laboratory of Dynamics and Control of Flight Vehicles, Beijing Institute of Technology, Beijing 100081, China
2 State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 200016, China
3 College of Mechanical Engineering, Beijing University of Technology, Beijing 100124, China
4 Xi’an Branch, China Academy of Space Technology, Xi’an 710100, China

More Information

Corresponding author: Hu Haiyan

摘要

摘要: 我国航天工业迫切需要掌握可入轨后展开的大型网架式空间结构技术，以便研制口径十几米、乃至数十米的大型星载天线。该技术的主要科学基础是这类空间结构展开和服役过程的非线性动力学建模、分析和控制。本文综述了与上述科学基础相关的研究进展，提出应重点关注的三个科学问题：一是大型网架式空间结构展开过程的多柔体系统动力学，尤其是如何对微重力环境下索网的接触和缠绕、运动副内碰撞、结构展开与航天器本体间的耦合等导致的非线性动力学进行建模和分析；二是大型网架式空间结构展开锁定后服役的动力学分析，尤其是如何揭示结构柔性、众多运动副间隙、交变热载荷等因素引起的复杂非线性振动机理；三是大型网架式空间结构展开锁定后服役的动力学控制，尤其是如何在欠驱动、低能耗条件下对非线性振动和波动传播提出有效的控制方法。
- 空间结构 /
- 展开 /
- 非线性动力学 /
- 多体系统动力学 /
- 振动控制 /
- 波动控制
Abstract: The space industry in China is eager to have the advanced technology of large space structures composed of trusses, cables and meshes. Such a large space structure, deployed on orbit, serves as the large antenna for different space missions. The important scientific basis of the technology is the nonlinear dynamic modeling, analysis and control of those space structures during their deployment and service. This review article surveys the advances in relevant researches and proposes three open problems as following. The first is the flexible multibody dynamics for the deployment of such a space structure, especially the nonlinear dynamic modeling and analysis for the contacts and wraps of mesh under microgravity, the internal impacts in clearance joints, and the coupling between structure deployment and spacecraft attitude. The second is the dynamic analysis of the space structures after deployment and during service, especially the complicated nonlinear vibrations of the flexible structure with numerous backlash joints under periodic thermal impacts. The third is the dynamic control of the space structures after deployment and during service, especially the under-actuated and lower-powered control for structure vibrations and waves.
- pace structure /
- deployment /
- nonlinear dynamics /
- multibody system dynamics /
- vibration control /
- wave control

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