复旦学报(自然科学版)2024,Vol.63Issue(6) :667-674.

基于动态逆的无人机自主着舰控制系统的设计与仿真

Design and Simulation of Autonomous Landing Control System for Unmanned Aerial Vehicle Based on Dynamic Inversion

邹锦 李一扬 艾剑良
复旦学报(自然科学版)2024,Vol.63Issue(6) :667-674.

基于动态逆的无人机自主着舰控制系统的设计与仿真

Design and Simulation of Autonomous Landing Control System for Unmanned Aerial Vehicle Based on Dynamic Inversion

邹锦 1李一扬 1艾剑良1
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作者信息

  • 1. 复旦大学航空航天系,上海 200433
  • 折叠

摘要

以如何使舰载无人机按照预定的着舰轨迹降落在航母上为研究背景,提出了一种基于动态逆设计的控制跟踪方法,建立了无人机的非线性6自由度模型,在着舰过程中加入舰尾流和航母运动的干扰,设计了动态逆控制器对着舰进行控制.仿真结果显示该着舰控制系统控制的无人机有很好的着舰成功率.

Abstract

Based on the research background of how a carrier-borne unmanned aerial vehicle(UAV)lands on an aircraft carrier according to a predetermined landing trajectory,a control tracking method based on dynamic inversion design is proposed.A nonlinear 6-degree-of-freedom model of the UAV is established.Interference from the wake of the ship and the movement of the aircraft carrier is added to the landing process.A dynamic inverse controller is designed to control the landing.The simulation results show good landing performance with a 98%success rate.

关键词

动态逆/舰尾流/着舰控制/舰载无人机

Key words

dynamic inversion/carrier air wake/landing control/carrier-borne unmanned aerial vehicle

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出版年

2024
复旦学报(自然科学版)
复旦大学

复旦学报(自然科学版)

CSTPCD北大核心
影响因子:0.388
ISSN:0427-7104
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