An Incremental Nonlinear Dynamic Inversion with Prescribed Performance for Damaged Aircraft

Yu Li, Xiaoxiong Liu, Qun Zuo, Wei Huang, Ruichen Ming, Weiguo Zhang

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

Abstract

This paper established a damaged aircraft model and developed a fault-tolerant controller based on incremental nonlinear dynamic inversion with prescribed performance to enhance flight safety. This fault-tolerant controller can rapidly stabilize the damaged aircraft, and tracking error is always within the prescribed boundaries in the whole process. Thus, the transient and steady-state performance of the damaged aircraft is guaranteed. Simulation results demonstrate that the developed fault-tolerant controller can achieve satisfactory control performance and improve aircraft flight safety.

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
Pages2024-2032
Number of pages9
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

  • Incremental nonlinear dynamic inversion
  • Prescribed performance
  • Robustness
  • Wing damage

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