EI、Scopus 收录
中文核心期刊

留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

考虑导轨间隙的在轨分离动力学计算方法

赵刚练 姜毅 陈余军 董晓彤

赵刚练, 姜毅, 陈余军, 董晓彤. 考虑导轨间隙的在轨分离动力学计算方法[J]. 力学学报, 2013, 45(6): 948-956. doi: 10.6052/0459-1879-13-193
引用本文: 赵刚练, 姜毅, 陈余军, 董晓彤. 考虑导轨间隙的在轨分离动力学计算方法[J]. 力学学报, 2013, 45(6): 948-956. doi: 10.6052/0459-1879-13-193
Zhao Ganglian, Jiang Yi, Chen Yujun, Dong Xiaotong. COMPUTATIONAL METHOD FOR DYNAMICS SIMULATION OF PAYLOAD SEPARATION FROM SATELLITE WITH RAIL CLEARANCE[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(6): 948-956. doi: 10.6052/0459-1879-13-193
Citation: Zhao Ganglian, Jiang Yi, Chen Yujun, Dong Xiaotong. COMPUTATIONAL METHOD FOR DYNAMICS SIMULATION OF PAYLOAD SEPARATION FROM SATELLITE WITH RAIL CLEARANCE[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(6): 948-956. doi: 10.6052/0459-1879-13-193

考虑导轨间隙的在轨分离动力学计算方法

doi: 10.6052/0459-1879-13-193
基金项目: 国家高技术研究发展计划资助项目(2012AA7042016).
详细信息
    通讯作者:

    赵刚练,博士,主要研究方向:发射动力学。E-mail:360185889@163.com

  • 中图分类号: O313.7;V412.4

COMPUTATIONAL METHOD FOR DYNAMICS SIMULATION OF PAYLOAD SEPARATION FROM SATELLITE WITH RAIL CLEARANCE

Funds: The project was supported by the National High Technology Research and Development Program of China (2012AA7042016).
  • 摘要: 传统在轨分离载荷动力学分析未考虑实际导轨的实时接触,无法准确分析分离时刻载荷的速度和角速度。针对半圆形双导轨,研究了空间导轨与定向器接触的特点及形式,基于分离装置的几何构型提出了一种确定发生相对轴向运动时导轨与定向器潜在接触对的方法,所提方法考虑了载荷轴线与导轨轴线的空间夹角,保证了分离后期接触检测的准确性,并可推广至多导轨接触计算。基于Lankarani与Nikravesh的连续接触力模型计算法向碰撞力,采用修正的Coulomb模型计算切向摩擦力。最后对飘浮基挠性航天器在轨分离载荷模型进行数值分析,验证了方法的有效性。结果表明导轨间隙增大了接触碰撞力,且随间隙的增大垂直于载荷分离方向的速度和角速度增大,导轨间隙使基座的转动与挠性附件强烈耦合,对航天器的稳定性造成影响。

     

  • Brown O, Eremenko P. Fractionated space architectures a vision for responsive space. The 4th Responsive Space Conference Paper RS4-2006-1002, 2006
    Wigbert F. Automated Rendezvous and Docking of Space-craft. Cambridge: Cambridge University Press, 2003
    张华, 肖余之, 徐博侯 等. 空间飞行器的对接分离与地面模拟试验的仿真分析研究. 宇航学报, 2008, (06): 1761-1765 (Zhang Hua, Xiao Yuzhi, Xu Bohou, et al. Analysis study on separation of aerospace vehicle and ground simulation test. Journal of Astronautics, 2008, (06): 1761-1765 (in Chinese))
    高有涛, 徐波, 陆宇平. 多星编队飞行的分散式耦合控制技术研究. 宇航学报, 2012, (09): 1248-1254 (Gao Youtao, Xu Bo, Lu Yuping. Decentralized coupled control for multi-satellite formation flight. Journal of Astronautics, 2012, (09): 1248-1254 (in Chinese))
    舒燕, 李志. 在轨释放、分离载荷动力学仿真研究. 航天器环境工程, 2012, (01): 18-22 (Shu Yan, Li Zhi. Dynamics simulation of on-orbit release and separation of payload. Spacecraft Environment Engineering, 2012, (01): 18-22 (in Chinese))
    沈晓凤, 肖余之, 康志宇. 小卫星偏心分离动力学仿真模型的建立与验证. 飞行力学, 2012, (03): 258-262 (Shen Xiaofeng, Xiao Yuzhi, Kang Zhiyu. Establishment and validation on dynamics simulation model of separation of eccentric sub-satellite. Flight Dynamics, 2012, (03): 258-262 (in Chinese))
    王功波, 郗晓宁, 刘磊. 小卫星编队在轨释放方案优化设计. 宇航学报, 2008, (02): 440-443 (Wang Gongbo, Xi Xiaoning, Liu Lei. Optimization on on-orbit release of small satellite formation flying. Journal of Astronautics, 2008, (02): 440-443 (in Chinese))
    姚世东. 考虑卫星推进剂晃动状态的卫星分离动力学分析. [硕士论文]. 湖南: 国防科学技术大学, 2006 (Yao Shidong. The separation dynamic analysis of the satellite considering the propellant-sloshing. [MS Thesis]. Hunan: National University of Defense Technology, 2006 (in Chinese))
    袁瑞. 航天器轨道机动动力学和分离动力学研究. [硕士论文]. 上海: 上海交通大学, 2009 (Yuan Rui. Investigation on the orbit maneuver dynamics and separation dynamics of spacecrafts. [MS Thesis]. Shanghai: Shanghai Jiaotong University, 2009 (in Chinese))
    Adams J, Robertson A, Zimmerman K, et al. Technologies for spacecraft formation flying. ION GPS-96 Conference, September, 1996. 1321-1330
    Bauer F, Bristow J, Folta D, et al. Satellite formation flying using an innovative autonmous control system (AutoCon) environment. In: Proc of AIAA/AAs Astrodynamics Specialists Conference, (New Orleans, LA), Aug, 1997. 657-666
    张磊. OTV在轨发射动力学建模与仿真. [硕士论文]. 湖南: 国防科学技术大学, 2007 (Zhang Lei. Modeling and simulation of OTV on-board launch. [MS Thesis]. Hunan: National University of Defense Technology, 2007 (in Chinese))
    蒋超, 王兆魁, 范丽 等. 卫星筒式偏心在轨分离动力学分析. 飞行力学, 2010, (01): 76-79 (Jiang Chao, Wang Zhaokui, Fan Li, et al. Dynamics analysis of the constrained and centroid biased on-orbit satellite separation. Flight Dynamics, 2010, (01): 76-79 (in Chinese))
    Jeyakumar D, Nageswara RB. Dynamics of satellite separation system. Journal of Sound and Vibration, 2006, 29(7): 444-455
    Flores P, Ambrosio J, Claro JCP, et al. Spatial revolute joints with clearances for dynamic analysis of multi-body systems. Journal of Multi-Body Dynamics, 2006, 220(4): 257-271
    Tian Q, Liu C, Machado M, et al. A new model for dry and lubricated cylindrical joints with clearance in spatial flexible multibody systems. Nonlinear Dynamics, 2011, 64(1-2): 25-47  
    游斌弟, 潘冬, 赵阳. 关节铰间隙对漂浮基星载天线扰动研究. 宇航学报, 2010, (10): 2251-2258 (You Bindi, Pan Dong, Zhao Yang. Research on disturbance of joint with clearance on free-floating satellite antenna. Journal of Astronautics, 2010, (10): 2251-2258 (in Chinese))
    Zhao Y, Bai ZF. Effects of clearance on deployment of solar panels on spacecraft system. Transactions of the Japan Society for Aeronautical and Space Sciences, 2011, 53(182): 291-295  
    Zhang LX, Bai ZF, Zhao Y, et al. Dynamic response of solar panel deployment on spacecraft system considering joint clearance. Acta Astronautica, 2012, 81: 174-185  
    Shaaban AA. Dynamics of Multibody System. 3rd edn. Chicago: Cambridge University Press, 2005. 267-308
    Lankarani HM, Nikravesh PE. A contact force model with hystersis damping for impact analysis of multibody systems. Journal of Mechanical Design, 1990, 112(3): 369-376  
    Lankarani HM, Nikravesh PE. Continuous Contact Force Models for Impact Analysis in Multibody Systems. Nonlinear Dynamics, 1994. 5(2): 193-207
    Ambrósio JAC. Impact of rigid and flexible multibody systems: Deformation description and contact models. In: Schiehlen W, Valášek M, eds. Virtual Nonlinear Multibody Systems. Berlin: Springer, 2003. 57-81
    段玥晨, 章定国, 洪嘉振. 作大范围运动柔性梁的一种碰撞动力学求解方法. 机械工程学报, 2012, 48(19): 95-102 (Duan Yuechen, Zhang Dingguo, Hong Jiazhen. Method for solving the impact problem of a flexible beam with large overall motion, Journal of Mechanical Engineering, 2012, 48(19): 95-102 (in Chinese))
    洪嘉振, 刘铸永. 变拓扑柔性多体系统接触碰撞动力学研究. 动力学与控制学报, 2013, 11(1): 5-7 (Hong Jiazhen, Liu Zhuyong. Study on contact/impact dynamics of flexible multibody system with topology variable. Journal of Dynamics and Control, 2013, 11(1): 5-7 (in Chinese))
  • 加载中
计量
  • 文章访问数:  1070
  • HTML全文浏览量:  75
  • PDF下载量:  682
  • 被引次数: 0
出版历程
  • 收稿日期:  2013-06-25
  • 修回日期:  2013-08-05
  • 刊出日期:  2013-11-18

目录

    /

    返回文章
    返回