| 飞机在风切变下进场的模拟试验研究 |
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| 引用本文： | 陈扬鉴,李翰芝.飞机在风切变下进场的模拟试验研究[J].飞行力学,1995,13(1):75-83. |
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| 作者姓名： | 陈扬鉴 李翰芝 |
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| 作者单位： | 西安飞行试验研究院 |
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| 摘 要： | 介绍在飞机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。
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| 关 键 词： | 飞机 风切变 着陆进场 模拟试验 |
SIMULATION EXPERIMENT AND INVESTIGATION OF AIRCRAFT IN LANDING APPROACH WITH WIND SHEAR |
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| Chen YangJian,Li Hanzhi, Lu Yuhu.SIMULATION EXPERIMENT AND INVESTIGATION OF AIRCRAFT IN LANDING APPROACH WITH WIND SHEAR[J].Flight Dynamics,1995,13(1):75-83. |
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| Authors: | Chen YangJian Li Hanzhi Lu Yuhu |
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| Institution: | Chinese Flight Test Establishment |
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| Abstract: | 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. |
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| Keywords: | Wind shear Landing approach Simulation experiment |
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