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飞机穿越微下击暴流起飞特性实时仿真研究
引用本文:孙宝亭 刘慧丰. 飞机穿越微下击暴流起飞特性实时仿真研究[J]. 飞行力学, 1993, 11(4): 57-62
作者姓名:孙宝亭 刘慧丰
作者单位:北京航空航天大学,北京航空航天大学 北京 100083,北京 100083
摘    要:
以大型客机为例,对飞机穿越微下击暴流的起飞飞行特性进行了实时数字,实时混合仿真及人机半物仿真研究,分析不同风场和不同进风高度对有,无人操纵飞行的航迹特性及相应状态变量响应特性的影响,探讨了飞机起飞飞行的安全性及正确操纵策略,最后给出了一些结论。

关 键 词:微下击暴流 起飞 安全性 实时仿真

REAL-TIME SIMULATION STUDY OF FLIGHT CHARACTER ISTICS FOR AIRCRAFT PENETRATING MICRO-DOWNBURST IN TAKE-OFF PHASES
Sun Baoting,Liu Huifeng. REAL-TIME SIMULATION STUDY OF FLIGHT CHARACTER ISTICS FOR AIRCRAFT PENETRATING MICRO-DOWNBURST IN TAKE-OFF PHASES[J]. Flight Dynamics, 1993, 11(4): 57-62
Authors:Sun Baoting  Liu Huifeng
Affiliation:Beijing University of Aeronautics and Astronautics
Abstract:
In the paper, the flight characterictics of aircraft penetrating microdownburst in take-off phases are studied by using methods of the real-time simulation, the methods including the real-time digital simulation, the real-time hybrid simulation and pilot-vehiele semi-physical simulation techniques. The flight trajectory of control and uncontrol and its response characteristics of the aircraft state variable are studied. The effects of the wind field intensity and into-wind height for aircraft safety are analyzed. The safety and its control countermeasure of the aircraft are explored. The conclusions helpful are obtained.
Keywords:Micro-downburst Take-off flight safety Control countermeasure Real-time simulation Pilot-vehiele semi-physical simulation.  
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