舰载机着舰航线侧方计时建模与分析

doi:10.3969/j.issn.1001-506X.2020.06.17

Abstract

Abstract:

For the sake of successful recovery of the embarked aircraft, the research of timing abeam is carried out to solve the problem of accurate distance on the downwind leg in the landing pattern. The glide slope distance of the aircraft can be extended for the motion of the sailing carrier, the ground velocity of the aircraft is naturally increased on the downwind leg and the flight path of the aircraft could be shifted when turning down in the landing pattern because of the natural wind. The factors above have great impact on recovery and should be taken into consideration, thus a model of the timing abeam for the aircraft on landing pattern is presented based on the flight dynamics theories and the numerical analysis is conducted with the model. The numerical simulation suggests that the method of the model is suitable for different types of the conventional take-off and landing fixed-wing carrier aircraft with different weights and munitions, and reasonable results can be obtained through the model.

Key words: embarked aircraft, landing pattern, timing abeam, model

CLC Number:

TP302.7

Kuizhi YUE, Jianzhong ZHAO, Liangliang CHENG, Dazhao YU. Analysis and modeling of timing abeam on landing pattern for embarked aircraft[J]. Systems Engineering and Electronics, 2020, 42(6): 1332-1337.

Figures/Tables 8

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References 30

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甲板合成风速/(m/s)	侧方计时时间t₁/s
15	12.4
14	13.2
13	13.9
12	14.7
11	15.5
10	16.4
9	17.2
8	18.1

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Analysis and modeling of timing abeam on landing pattern for embarked aircraft

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