重复折展锁解式太阳翼多体系统动力学建模与分析

胡明; 孔菲; 陈文华; 李文娟; 撖亚頔; 王庆九

doi:10.11728/cjss2014.04.489

重复折展锁解式太阳翼多体系统动力学建模与分析

doi: 10.11728/cjss2014.04.489 cstr: 32142.14.cjss2014.04.489

1.
浙江理工大学浙江省机电产品可靠性技术研究重点实验室杭州 310018
2.
浙江大学机械工程系杭州 310027

基金项目: 国家自然科学基金项目（51375458，51006134），浙江省自然科学基金项目（LZ12E05004），国防技术基础项目，教育部高校博士点基金优先发展项目（20123318130001），浙江省重点科技创新团队计划项目（2010R50005）和航天支撑技术基金项目共同资助

详细信息

通讯作者:

胡明,E-mail:huming@zstu.edu.cn

中图分类号: V423.4
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出版历程
- 收稿日期: 2013-09-30
- 修回日期: 2014-03-19
- 刊出日期: 2014-07-15

Multi-body Dynamics of Repeated Fold-unfold and Lock-unlock Solar Array

1.
Zhejiang Province's Key Laboratory of Reliability Technology for Mechanical and Electrical Products, Zhejiang Sci-Tech University, Hangzhou 310027
2.
Department of Mechanical Engineering, Zhejiang University, Hangzhou 310027

摘要

摘要: 为研究重复折展锁解式太阳翼展开力学特性，针对其有根树链式拓扑结构特点，依据一阶模态刚度分析假设模型，由Jourdain变分原理建立太阳翼树形柔性多体系统动力学理论模型；结合太阳翼关节铰机构运动规律，采用单向递推组集建模方法构建太阳翼展开过程正逆混合动力学模型；基于重复折展锁解式太阳翼结构参数和物理性能参数进行数值仿真，研究蜂窝夹层复合式基板柔性结构对太阳翼展开力学规律的影响，得到太阳翼各基板质心运动规律及其展开过程所需施加的驱动力矩. 所得结果可较好地预测太阳翼展开过程的动态行为，为其后续工程应用提供依据.
- 太阳翼 /
- 柔性多体系统 /
- 重复折展锁解机构 /
- 变分原理 /
- 展开动力学
Abstract: This paper presents the dynamic characteristics of repeated fold-unfold and lock-unlock solar array, which is in a topological tree configuration. According to the first modal stiffness analysis, assumptions about solar array multi-body system are proposed. Deduced from Jourdain variation principle, dynamic model of solar array flexible multi-body system is built. Furthermore, the forward-inverse mixed dynamic model is established through forward recursive formulation and motion law of solar array hinges. In order to study the impact of flexible structures on solar array deployment, the motion parameters of solar array panels, such as rotation angle, angular velocity and angular acceleration, are obtained from numerical simulation, which is based on the structure and physical parameters of repeated fold-unfold and lock-unlock solar array prototype. The results can well predict dynamic behaviors of solar array during its deploying process. In conclusion, this study has laid a foundation for subsequent engineering applications of repeated fold-unfold and lock-unlock solar array.
- Solar array /
- Flexible multi-body system /
- Repeated fold-unfold and lock-unlockmechanism /
- Variation principle /
- Deployment dynamics

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参考文献(13)

[1]	Yuan Jiajun. Design and Analysis of Satellite Structures[M]. Beijing: China Astronautic Publishing House, 2009: 210-269. In Chinese (袁家军. 卫星结构设计与分析[M]. 北京: 中国宇航出版社, 2009: 210-269)
[2]	Wie B, Furumoto N, Banerjee A K. Modeling and simulation of spacecraft solar array deployment[J]. J. Guid. Control Dynam., 1986, 9(5):593-598
[3]	Yasushi K, Shigemune T, Yoshiaki O. Dynamic simulation of stick-slip motion of a flexible solar array[J]. Spec. Sect. Large Scale Syst., 2008, 16(6):724-735
[4]	Oskar W, Simon W. Simulation of deployment of a flexible solar array[J]. Multibody Syst. Dyn., 2002, 7:101-125
[5]	Gina M O, Thomas M, Grant T. Free deployment dynamics of a z-folded solar array[C]//52nd AIAA/A-SME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Denver: AIAA, 2011: 1730-1736
[6]	Zhou Zhicheng, Qu Guangji. Multi-body dynamics of spacecraft solar wing[J]. Mech. Eng., 1990(6):53-57. In Chinese (周志成, 曲广吉. 航天器太阳阵多体展开的动力学分析[J]. 力学与实践, 1990(6):53-57)
[7]	Wang Ensong. Deployment dynamics of solar array[J]. J. Beijing Univ. Aeron. Astron., 1994, 20(4):446-451. In Chinese (汪恩松. 卫星太阳阵展开的动力学方程[J]. 北京航空航天大学学报, 1994, 20(4):446-451)
[8]	Qiu Zhicheng. Active vibration control for coupling system of flexible structures and rigid body[J]. Chin. J. Mech. Eng., 2006, 42(11):26-33. In Chinese (邱志成. 刚柔耦合系统的振动主动控制[J]. 机械工程学报, 2006, 42(11):26-33)
[9]	You Bindi, Wang Xinggui, Chen Jun. Vibration and impact for deployable solar array of satellite with locking hinges[J]. J. Mech. Eng., 2012, 48(21):67-76. In Chinese (游斌弟, 王兴贵, 陈军. 卫星太阳阵展开锁紧过程冲击振动[J]. 机械工程学报, 2012, 48(21):67-76)
[10]	Jones P A, Spence B R. Spacecraft solar array technology trends[J]. Aerosp. Elec. Syst. Mag., 2011, 26(8):17-28
[11]	Kojimaa Y, Taniwakib S, Okami Y. Dynamic simulation of stick-slip motion of a flexible solar array[J]. Contr. Eng. Pract., 2008, 16(6):724-735
[12]	Li Dongxun. Structural Dynamics of Flexible Spacecraft[M]. Beijing: Science Press, 2010: 189-216. In Chinese (李东旭. 挠性航天器结构动力学[M]. 北京: 科学出版社, 2010: 189-216)
[13]	Hong Jiazhen. Computational Multibody Dynamics[M]. Beijing: Higher Education Press, 2003: 329-408. In Chinese (洪嘉振. 计算多体系统动力学[M]. 北京: 高等教育出版社, 2003: 329-408)