Moving path following with integrated direct lift control for carrier landing

被引：20

作者：

Guan, Zhiyuan ^{[1
]}

Liu, Hu ^{[1
]}

Zheng, Zewei ^{[2
]}

Ma, Yunpeng ^{[1
]}

Zhu, Tiefu ^{[3
]}

机构：

[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China

[2] Beihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Beijing 100191, Peoples R China

[3] AVIC Shenyang Aircraft Design & Res Inst, Shenyang 110087, Peoples R China

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2022年 / 120卷

基金：

中国国家自然科学基金; 北京市自然科学基金;

关键词：

Automatic carrier landing; Disturbance observer; Integrated direct lift control; Moving path following; UNMANNED AERIAL VEHICLES; PRESCRIBED PERFORMANCE;

D O I：

10.1016/j.ast.2021.107247

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper addresses the three dimensional moving path following (MPF) problem, where a vehicle is required to follow a path attached to a moving target in three dimensional space. The MPF problem is divided into guidance and attitude control. For guidance, a non-singular three dimensional MPF law is proposed. For attitude control, a novel integrated direct lift control method is demonstrated to response to the guidance commands. The idea of using direct lift improves the control performance of a fixed-wing aircraft. In addition, both of the MPF law and the integrated direct lift control method are utilized to design the flight controller for automatic carrier landing, which is a typical MPF mission. Finally, the theoretical analysis and numerical simulation verify the advantages of the proposed controller. (C) 2021 Elsevier Masson SAS. All rights reserved.

引用

页数：15

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