考虑杆臂效应与挠曲变形的全自动着舰技术

doi:10.7527/S1000-6893.2021.25841

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考虑杆臂效应与挠曲变形的全自动着舰技术

梁磊^1,2, 肖静¹, 詹光¹, 苏大林¹

1. 航空工业沈阳飞机设计研究所, 沈阳 110031;
2. 中国航空研究院研究生院, 扬州 225002

收稿日期:2021-04-15 修回日期:2021-05-08 发布日期:2021-05-31
通讯作者: 梁磊 E-mail:liangleinwpu@yeah.net

Automatic landing technology considering lever arm effect and flexural deformation

LIANG Lei^1,2, XIAO Jing¹, ZHAN Guang¹, SU Dalin¹

1. AVIC Shenyang Aircraft Design and Research Institute, Shenyang 110031, China;
2. Chinese Aeronautical Establishment Graduate School, Yangzhou 225002, China

Received:2021-04-15 Revised:2021-05-08 Published:2021-05-31

摘要/Abstract

摘要： 联合精确进近和着陆系统（JPALS）舰载组件旨在为最终进近阶段的舰载机提供自动着舰能力。针对由于舰船杆臂效应与挠曲变形的存在导致舰载机着舰定位精度下降的问题，开发了一种基于卫星引导的全自动着舰非线性化参数误差模型，结合舰船甲板运动及舰载机纵向飞行控制模型，评估舰船结构挠曲和姿态不确定性对着舰落点精度的影响。结果表明，杆臂效应与挠曲变形对着舰落点精度有显著影响，利用建立的误差模型以及飞行控制模型，能够将着舰落点精度有效控制在着舰标准之内。

关键词: JPALS, 杆臂效应, 挠曲变形, 非线性化, 着舰落点精度

Abstract: The shipboard components of the Joint Precision Approach and Landing System (JPALS) are designed to provide automatic landing capability for the carrier-based aircraft in the final approach phase. However, the landing accuracy of the carrier-based aircraft is reduced due to the existence of ship's lever arm effect and flexible deformation. In this paper, a nonlinear parameter error model is developed based on satellite guided automatic landing. The model is used with the ship deck motion and longitudinal flight control model to evaluate the influence of ship structure deflection and attitude uncertainty on aircraft landing accuracy. The results show that the lever arm effect and flexible deformation have a significant impact on the landing accuracy. Using the error model proposed and the flight control model, the accuracy of the landing point can be effectively controlled within the landing standard.

Key words: joint precision approach and landing system (JPALS), lever arm effect, flexural deformation, nonlinear, landing accuracy

中图分类号:

V249.1

梁磊, 肖静, 詹光, 苏大林. 考虑杆臂效应与挠曲变形的全自动着舰技术[J]. 航空学报, 2021, 42(8): 525841-525841.

LIANG Lei, XIAO Jing, ZHAN Guang, SU Dalin. Automatic landing technology considering lever arm effect and flexural deformation[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525841-525841.

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E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

考虑杆臂效应与挠曲变形的全自动着舰技术

Automatic landing technology considering lever arm effect and flexural deformation

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