| 引用本文: | 葛玉君,秦子增.可控翼伞系统的滑翔与稳定性分析.[J].国防科技大学学报,1992,14(4):34-39.[点击复制] |
| Ge Yujun,Qin ZiZeng.Analyses of Glide and Stability Performance of Controllable Parafoil Systems[J].Journal of National University of Defense Technology,1992,14(4):34-39[点击复制] |
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| 可控翼伞系统的滑翔与稳定性分析 |
| 葛玉君, 秦子增 |
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(航天技术系)
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| 摘要: |
| 可控翼伞系统在飞行器回收领域有广阔的应用前景。本文就可控翼伞系统建立了六自由度数学模型，并用该模型对40m2可控翼伞系统的滑翔和稳定性进行了仿真计算和分析，研究结果对可控翼伞系统设计和实验有一定参考价值。 |
| 关键词: 可控翼伞，系统，滑翔，仿真 |
| DOI： |
| 投稿日期：1991-12-10 |
| 基金项目: |
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| Analyses of Glide and Stability Performance of Controllable Parafoil Systems |
| Ge Yujun, Qin ZiZeng |
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(Department of Aerospace Technology)
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| Abstract: |
| The development of a controllable parafoil system provides the prospects for precise，undamagea recovery of large delicate payloads and recovery return systems intended for reuse. In this paper a six-degree-of-freedom flight dynamics model for such a system is presented and the simulation program is developed to aid the study of system performance such as glide and dynamic stability etc. As an example，the glide and dynamic stability performance of 40 (sqm) are a parafoil system has been discussed and some satisfactory results were obtained. |
| Keywords: simulation,controllable parafoil,system,glide |
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