测控技术2013，Vol.32Issue(2)：51-55,5.
基于CFD方法的动力伞雀降控制优化研究
Research on the Optimization of Flare Maneuver Control of the Powered Parachute Based on CFD
摘要
Abstract
The main factors of sparrow performance are researched aim at the flare maneuver of powered parachute, and the reasonable control laws are summarized based on a lot of experimental results. The longitudinal model of the powered parachute as the foundation, using dynamic mesh technique, the classic processes of flare maneuver are simulated dynamically in FLUENT, the influence of flow angle of attack, the manipulating trip and the manipulating speed on the performance of the flare maneuver is researched. The experimental results show that the trip and pull-down speed are the main factors to affect the performance of the flare maneuver. The analysis indicates the best flare maneuver time and control law are obtained, the control strategy is optimized and a basis is provided for powered parachute aerodynamic analysis combined with the actual control.关键词
动力伞/雀降/动网格/控制优化Key words
powered parachute/ flare maneuver/ dynamic mesh/ control optimization分类
信息技术与安全科学引用本文复制引用
陈自力,张昊..基于CFD方法的动力伞雀降控制优化研究[J].测控技术,2013,32(2):51-55,5.基金项目
国防武器装备预研基金资助项目 （）
