伞-载系统拉直过程动力学仿真研究进展
DOI:
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:


Review of Deployment Research on Dynamics Simulation of Parachute-Payload System
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    降落伞拉直过程是关系到伞-载系统安全可靠工作的关键阶段,涉及到三维空间多体系统动力学和变质量变自由度动力学问题。本文综述了柔性降落伞拉出过程动力学仿真技术中的一些关键问题。首先从拉直过程仿真方法进行介绍,通过具体 算例分析了各自方法的特点。然后构建了动力学模型中主要因素之间的相互关系,分析了气 动力的影响因素及风速对拉出过程的影响。同时阐述了绳段张力的几种计算模型及其特点,指出 了它们的一般应用范围。最后,对伞-载系统拉直过程仿真减小数值计算误差的途径及未来需要 关注的几个方面进行了探讨。

    Abstract:

    The parachute deployment process is the key stage to ensure the safety and reliability of parachute-payload system. The deployment system is a complex non-linear dynamic system involved in variable quality and freedoms of three-dimensional multi-body objects. Some key problems of flexible parachute deployment dynamic simulation technology are discussed. The simulation methods are introduced at first and the characteristics of each method are analyzed by actual numerical examples. Then, the relationship between main factors of deployment dynamic model is constructed and the influence of wind velocity on deployment process is analyzed. Moreover, some tension model and their features are given, and the application ranges of these tension models are pointed out. Finally, several problems of parachute deployment simulation are proposed, such as the way to decrease the error and some ones that should be taken into account in the future.

    参考文献
    相似文献
    引证文献
引用本文

余莉史献林.伞-载系统拉直过程动力学仿真研究进展[J].南京航空航天大学学报,2016,48(4):454-462

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2016-09-08
  • 出版日期:
文章二维码
您是第位访问者
网站版权 © 南京航空航天大学学报
技术支持:北京勤云科技发展有限公司