期刊文献+
任意字段
题名或关键词
题名
关键词
文摘
作者
第一作者
机构
刊名
分类号
参考文献
作者简介
基金资助
栏目信息

翼伞空投操纵绳拉动过程中的位置解算 被引量：2

Position Prediction of Parafoil in Control Rope Pulling Course
在线阅读 下载PDF
导出
摘要 通过翼伞系统的刚性特性出发,提出了一种基于微元分析的翼伞操纵绳拉动过程中的运动位置解算方法,有利于提高翼伞空投的精度。 The rigid character of parafoil was analyzed. A position prediction method based on differential coefficient for parafoil control rope pulling course was put forward. The purpose was to improve air drop precision.
作者 李良春 蒲志刚 唐波
机构地区 总装军械技术研究所 军械工程学院
出处 《包装工程》 CAS CSCD 北大核心 2009年第12期104-105,共2页 Packaging Engineering
关键词 翼伞 空投 操纵绳 位置解算 parafoil airdrop control rope position prediction
分类号 E234 [军事—军事理论]
作者简介 李良春（1967-），男，四川广安人，博士，总装军械技术研究所高级工程师，主要从事军用包装研究。
  • 相关文献

参考文献5

二级参考文献18

  • 1Mcvey D F, Wolf D F. Analysis of Deployment and Inflation of Large Ribbon Parachute. J. Aircraft, 1974, 11(2): 96-103.
  • 2Sundberg W D. Status Report: Parachute System Design, Analysis and Simulation Tool. AIAA 93-1208.
  • 3Purvis J W. Prediction of LineSail During Lines-First Deployment. AIAA 83-0370.
  • 4Moog P D. Aerodynamic Line Bowing Parachute Deployment. AIAA75-1381.
  • 5Srinivas E K, Modeling Issues Related to Retrieval Flexibale Tethered Satellite Systems. J. of Guidance Control and Dynamics, 1995, 18 (5): 1169-1176.
  • 6Huston R L, Kamman J W. A representation of fluid forces in finite segment cable models. Computer & Structure. 1981, 14 (4) 281-287.
  • 7Banerjee A K, Van N Do. Deployment Control of a Cable Connecting a Ship to an Underwater Vehicle. J. of Guidance control and Dynamics, 1994, 17 (6): 1327-1332.
  • 8Djerassi S, Bambergers H. Simultaneous Deployment of a Cable from Two Moving Platforms. J. of Guidance Control and Dynamics , 1998, 21 (2): 271-276.
  • 9Geoffrey F, Costello M. Improved Deployment Characteristics of Tether-Connected Munition Systems. J. of Guidance Control and Dynamics, 2001, 24 (3): 547-554.
  • 10Cheng Wenke. Dynamics and dyamic stability analysis of general parachute-load system, phD thesis, Nation University of Defense Techndogy, 2000.

共引文献27

同被引文献17

  • 1熊菁,秦子增,文红武.翼伞系统归航的最优控制[J].航天控制,2004,22(6):32-36. 被引量：8
  • 2杨杰,赵敏,姚敏,等.翼伞自主归航系统关键技术发展研究[C].IEEEChineseGuidance,NavigationandControlConference,烟台:北京航空航天大学,2014.
  • 3A. Rosich, P. Gurfil." Coupling in-flight trajectory planning and flocking for muhiple autonomous parafoils" [ J ]. Pro- ceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2012: 691.
  • 4Branden J. Rademacher, Ping Lu, Alan L. Strahan, etc. Journal of guidance, control, and dynamics [ J ]. Vol. 32, NO.6, November-December 2009.
  • 5Limin Zhang, Haitao Gao et al. " Multi-objective global optimal parafoil homing trajectory optimization via Gauss pseudospectral method" [ J ]. Nonlinear Dyn, 2013,72 : 1-8.
  • 6L. Yili, L. Huabao. "Theoretical investigation of gliding parachute trajectory with deadband and non-proportional automatic homing control" [ R] .AIAA-91-0834,1991.
  • 7Scott Dellicker, Richard Benney, Glen Brown. Guidance and Control for Flat-Circular Parachutes [ J ]. Journal of Aircraft, 2001,38 ( 5 ).
  • 8Rosich A,Gurfil P.Coupling in-flight Trajectory Planning and Flocking for Multiple Autonomous Parafoils[J].Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering,2012,226:691-720.
  • 9Scott Dellicker,Richard Benney,Glen Brown.Guidance and Control for Flat-Circular Parachutes[J].Journal of Aircraft,2001,(32):110-120.
  • 10Li Y,Lin H.Theoretical Investigation of Gliding Parachute Trajectory With Deadband and Non-Proportional Automatic Homing Control[C].AIAA Aerodynamic Decelerator Systems Technology Conference,11 th,San Diego,CA,1991:42-47.

引证文献2

二级引证文献6

包装工程
2009年 第12期

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
关于我们 | 版权声明 | 联系我们 | 帮助中心| 意见反馈
主办单位：上海市教育委员会
技术支持：重庆维普资讯有限公司
渝公网安备 50019002500403号
使用帮助 返回顶部