摘要
在飞行器回收领域,应用可控翼伞代替降落伞,是实现飞行器有效载荷定点无损着陆的一项高技术。本文就可控翼伞系统建立了六自由度模型。用该模型对40m^2可控翼伞系统的转弯控制特性进行了仿真计算和分析。
Development of a controllable parafoil system provides the potential for precise undamaged recovery of large delicate payloads. In this paper, a six-degree-of-freedomflight dynamics model for controllable parafoil systems was presented and the simulation program was developed to aid study of system performance such as response to turn control. As an example, flight turn performance of a 40(sqm) area parafoil system was discussed and some satisfactory results to design and test parafoil system were obtained.
出处
《宇航学报》
EI
CAS
CSCD
北大核心
1993年第1期89-96,共8页
Journal of Astronautics
关键词
可控翼伞
仿真
转弯控制
降落伞
Controllable parafoil, Simulation, Turn control.
