基于飞行模拟的超低空空投操控方法研究  

作　　者：雒东超 张晓敏[1] 王文星[1] 

机构地区：[1]中国飞行试验研究院

出　　处：《科技创新导报》2019年第24期10-13,15,共5页Science and Technology Innovation Herald

摘　　要：根据飞行试验模拟验证的需要,基于分离体法, 建立了超低空重装空投的过程模型, 并同时建立了牵引伞模型,构 建了较为完善的超低空重装空投飞行仿真环境。根据人在回路的超低空重装空投仿真试验结果,提出了超低空重装空投 过程的任务流程和驾驶员操控方法。所得结论对空投过程驾驶员操控和任务的顺利进行具有重要的参考价值。In this paper,according to the needs of the f light test of simulation,Based on the separation body method,the ultra-low altitude heavyweight airdrop model was developed,the extraction parachute model was developed as well which made the ultra-low altitude heavyweight airdrop f light simulation environment much more perfect.According to the pilot-in-the-loop f light simulation results,the mission process and pilot’s handle method was given out.The results show that the method in this paper has important reference value for pilot’s handling and ultra-low airdrop mission.

关 键 词：超低空 重装空投 飞行模拟 操控方法 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]