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Direct Lift Control of Carrier-Based Aircraft Based on Thrust Vector

  • Xiulin Zhang
  • , Jiaxing Wang
  • , Xinyu Feng
  • , Zheng Shao
  • , Jingping Shi
  • Shenyang Institute of Aircraft Design and Research

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Scopus citations

Abstract

When the carrier-based aircraft in the landing stage, it will be affected by the complex sea conditions and ship wake disturbances, the accident rate at this stage is higher than ever. Therefore, the carrier-based aircraft needs to quickly track the glide path command, and stabilize the angle of attack to maintain lift. Aiming at this problem, this paper designs a direct lift control method based on thrust vector. By modeling the vector engine, the physical quantities of the thrust vector acting on the aircraft are deduced, and then the direct lift landing control law of the carrier aircraft is designed. Based on MATLAB software simulation verification, the results show that the direct lift control method based on the thrust vector can better track the glide path command, realize the safe and accurate landing of the carrier-based aircraft.

Original languageEnglish
Title of host publicationAdvances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
EditorsLiang Yan, Haibin Duan, Yimin Deng, Liang Yan
PublisherSpringer Science and Business Media Deutschland GmbH
Pages1750-1759
Number of pages10
ISBN (Print)9789811966125
DOIs
StatePublished - 2023
EventInternational Conference on Guidance, Navigation and Control, ICGNC 2022 - Harbin, China
Duration: 5 Aug 20227 Aug 2022

Publication series

NameLecture Notes in Electrical Engineering
Volume845 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Guidance, Navigation and Control, ICGNC 2022
Country/TerritoryChina
CityHarbin
Period5/08/227/08/22

Keywords

  • Carrier-based aircraft control
  • Direct lift control
  • Landing control
  • Simulation analysis
  • Thrust vector technology

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