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Aircraft Intelligent Guidance Technology for Evasion and Penetration

  • Jinbai Li
  • , Honglun Wang*
  • , Yiheng Liu
  • , Tiancai Wu
  • *Corresponding author for this work
  • Beihang University

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

Abstract

In this paper, in order to improve the performance of aircraft evasion and penetration, an intelligent guidance algorithm is proposed by combining twin delayed deep deterministic policy gradient (TD3) and interfered fluid dynamical system (IFDS). First, the guidance model and simulation environment are established. On this basis, the basic guidance algorithm IFDS and the deep reinforcement learning method TD3 are introduced respectively, and the intelligent guidance algorithm is designed. Then, this paper compares and analyzes the simulated flight path of the aircraft obtained by the traditional guidance algorithm and the intelligent guidance algorithm. Finally, simulations show that the intelligent guidance algorithm can guide the aircraft to avoid obstacles and missiles, and demonstrate the advantages of the intelligent guidance algorithm.

Original languageEnglish
Title of host publicationProceedings of 2021 International Conference on Autonomous Unmanned Systems, ICAUS 2021
EditorsMeiping Wu, Yifeng Niu, Mancang Gu, Jin Cheng
PublisherSpringer Science and Business Media Deutschland GmbH
Pages1913-1922
Number of pages10
ISBN (Print)9789811694912
DOIs
StatePublished - 2022
EventInternational Conference on Autonomous Unmanned Systems, ICAUS 2021 - Changsha, China
Duration: 24 Sep 202126 Sep 2021

Publication series

NameLecture Notes in Electrical Engineering
Volume861 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Autonomous Unmanned Systems, ICAUS 2021
Country/TerritoryChina
CityChangsha
Period24/09/2126/09/21

Keywords

  • Aircraft intelligent avoidance
  • Deep reinforcement learning
  • Intelligent guidance algorithm
  • Interfered fluid dynamical system

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