期刊文献+

空间含铰可展桁架结构的非线性动力学建模与分析 被引量:7

Nonlinear Dynamic Modeling and Analysis for Space Deployable Structure with Clearance Joints
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摘要 综合考虑间隙、非线性刚度、摩擦及碰撞阻尼,建立了铰链等效模型,并基于该等效模型建立了含铰可展桁架结构动力学模型。根据铰链的变拓扑结构特点,提出了适用于解决时变非线性动力学问题的附加力方法,对多自由度平面和空间可展桁架进行了动力学仿真,得到了可展桁架的动力学响应。通过设置不同铰链参数和外部激振条件,分析了不同间隙、激振力、摩擦力对含铰可展桁架频率和幅值的影响,结果表明:间隙和激振力增大可导致桁架固有频率降低,响应幅值增大;摩擦力增大可提高桁架的固有频率。多单元桁架伸展臂的动力学试验结果验证了文中建立的含铰可展桁架动力学模型的正确性。 An equivalent model of clearance joints is presented by considering clearance,nonlinear stiffness,friction and impact damping.And a nonlinear dynamic model of the space deployable structure is established on the basis of the equivalent model.According to the variable topology characteristics,an additional force method is proposed to solve the nonlinear dynamic equation of the clearance joint structure.Dynamic simulations of the plane and space structures with clearance joints are conducted.Changing joint parameters and vibration condition,the effects of joint clearance,exciting force and friction force on the structure are analyzed.The results show that the natural frequency'lowers and the amplitude of response magnifies with the increasing clearance size and exciting force,while the natural frequency rises with the increasing friction force.Dynamics experiment of deployable articulated mast verifies the correctness of the model of deployable structure with clearance joints.
出处 《西安交通大学学报》 EI CAS CSCD 北大核心 2013年第11期113-119,126,共8页 Journal of Xi'an Jiaotong University
基金 国家自然科学基金重点资助项目(50935002) 国家青年科学基金资助项目(11002039)
关键词 可展桁架结构 间隙铰 非线性动力学 建模 deployable structure clearance joint nonlinear dynamics modelling
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参考文献20

  • 1FERNANDEZ J M,LAPPAS V J,DATON-LOVETT A J.Completely stripped solar sail concept using bistable reeled composite booms[J].Acta Astronautica,2011,69:78-85.
  • 2BROWN M A.A deployable mast for solar sails in the range of 100-1000 m[J].Advances in Space Research,2011,48:1747-1753.
  • 3田大可,刘荣强,邓宗全,郭宏伟.多模块构架式空间可展开天线背架的几何建模[J].西安交通大学学报,2011,45(1):111-116. 被引量:7
  • 4MEGURO A,SHINTATE K,USUI M,et al.In-orbit deployment characteristics of large deployable antenna reflector onboard Engineering Test Satellite Ⅷ[J].Acta Astronautica,2009,65:1306-1316.
  • 5郭宏伟,刘荣强,邓宗全.空间索杆铰接式伸展臂性能参数分析与设计[J].北京航空航天大学学报,2008,34(10):1186-1190. 被引量:19
  • 6文荣,吴德隆.空间伸展机构动力学实验研究[J].导弹与航天运载技术,1996(2):4-13. 被引量:8
  • 7MOON F C,LI G X.Experimental study of chaotic vibrations in a pin-jointed space truss structure[J].AIAA Journal,1990,28(5):915-921.
  • 8FERRI A A.Modeling and analysis of nonlinear sleeve joints of large space structures[J].AIAA Journal,1988,25(5):354-360.
  • 9DUBOWSKY S,FREUDENSTEIN F.Dynamic analysis of mechanical systems with clearances:part 1 formation of dynamic model[J].Journal of Engineering for Industry,1971,93(1):305-309.
  • 10DUBOWSKY S,FREUDENSTEIN F.Dynamic analysis of mechanical systems with clearances:part 2 dynamic response[J].ASME Journal of Engineering for Industry,1971,93(1):310-316.

二级参考文献44

  • 1苏斌,关富玲,杨大彬,杨治.索杆式伸展臂的展开驱动设计与动力学分析[J].空间科学学报,2004,24(4):312-320. 被引量:10
  • 2张淑杰,李瑞祥,丁同才.盘绕式杆状展开机构的设计与力学分析[J].力学季刊,2006,27(2):341-347. 被引量:11
  • 3乐英,韩庆瑶,王璋奇.数控加工中非圆曲线的最小二乘圆弧逼近[J].华北电力大学学报(自然科学版),2006,33(6):102-104. 被引量:15
  • 4吴德隆 阎绍泽 黄铁球 张永.空间大型伸展机构动力学研究[A].陈滨主编.动力学振动与控制的研究[C].长沙:湖南大学出版社,1998.239—245.
  • 5SRTM hardware-the mast: Payload bay[ EB/OL]. Shuttle Press Kit, 2000-01-18. http://www, shuttlepressklt, com/STS -99/ playload57. htm
  • 6Levine M B. Microdynamic behavior of a joint dominated structure on-orbit[R]. AIAA-99-1267, 1999
  • 7Farr T G, Rosen P A. The shuttle radar topography mission[R/ OL]. http ://trs-new. jpl. nasa. gov
  • 8Crawford R F. Strength and efficiency of deployable booms for space applications[ R]. AIAA-1971-396, 1971
  • 9Boom information [ EB/OL 5- AEC-Able Engineering Company Inc, 2004. http://www, aec-able, corn
  • 10Murphey T W. A material structure performance index for strain based deployable trusses[R]. AIAA-2004-1656, 2004

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