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引导伞减速伞开伞过程建模 被引量:5

Modeling Deployment of Pilot and Drogue Parachute
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摘要 侧风情况下展开减速系统存在着一定的风险 ,如果系统不按最小绳帆设计 ,会导致降落伞系损坏的后果。文章介绍了引导伞减速伞的开伞过程建模及应用分析代码 (RVAC)和图形动画 (DISPLAY)的实例。 There are some risks in deployment of decelerating system when the crosswind exists. So the parachutes maybe get hurt if the system was not designed by minimal sail length theory. This paper describes how to model the deployment of pilot and drogue parachutes, introduces some examples using Reentry Vehicle Analysis Code (RVAC) and animation software (DISPLAY).
作者 沈祖炜 黄伟
出处 《航天返回与遥感》 2005年第1期27-35,共9页 Spacecraft Recovery & Remote Sensing
关键词 再入飞行器 回收系统 引导伞 减速伞 Reentry aircraft Recovery system Pilot Drogue
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参考文献4

  • 1Purvis J. W. Prediction of Parachute Line Sail during Line First Deployment. Journal of Aircraft, 1983,20( 11 ).
  • 2Purvis J. W. Improved Prediction of Parachute Line Sail During Line - First Deployment. A1AA84 - 0786,1984.
  • 3W. D. Sundberg. Parachute System Design, Analysis and Simulation Tool. AIAA93- 1208.1993.
  • 4E.K.Srinivas. Modeling Issues Related to Retrieval Flexible Tethered Satallite Systems. Guidance Control and Dynamics 1995:1169-1176.

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