摘要
介绍在飞行轨迹稳定性指标模拟试验中所用的有风切变时的数学模型。在地面模拟试验中采用着陆进场的人－机闭环控制方法，开展驾驶员定量评价，给出试验结果。对国军标ＧＪＢ１８５－８６的这一指标要求提出修改建议。讨论了在风切变下着陆进场的特性和驾驶技术。试验结果正确可靠，可作为飞机设计、飞行试验和修订我国军用规范的重要依据。
Mathematical models with wind shear in use for simulation experiment offlight path stability specificafion are presented.A method of pilot-vehicle closed-loopcontrol in approach is used in the ground simulation experiment.The pilot quantitative ratingis developed. Their experiment results are given.Revision to the specification requirement inGJB 185-86 is proposed. Landing approach characteristics and pilot techniques on the windShears are discussed.The results are correct and are relied upon. They can be used as important basis ofaircraft design, night test and revision to the specification requirement in GJB 185-86.
出处
《飞行力学》
CSCD
北大核心
1995年第1期75-83,共9页
Flight Dynamics
关键词
飞机
风切变
着陆进场
模拟试验
Wind shear Landing approach Simulation experiment
