Flight Attitude Control of an Electric Vertical Takeoff and Landing with Flexible Frame

Yu Zhang, Wei Fan*, Bin Xu, Changle Xiang, Hua Zhu, Xing Yue

*Corresponding author for this work

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

1 Citation (Scopus)

Abstract

The stability problem of an Electric Vertical Takeoff and Landing (eVTOL) aircraft with flexible frame is investigated in this paper. A spring damping model is adopted to describe the deformation of the frame of eVTOL, where modeling and parameter uncertainties are considered. Based on the L1 output feedback algorithm, an adaptive controller is proposed to augment the stability of the eVTOL system. Numerical simulation is conducted to illustrate the effectiveness and feasibility of the theoretical results..

Original languageEnglish
Title of host publicationCSAE 2021 - Proceedings of the 5th International Conference on Computer Science and Application Engineering
EditorsAli Emrouznejad
PublisherAssociation for Computing Machinery
ISBN (Electronic)9781450389853
DOIs
Publication statusPublished - 19 Oct 2021
Event5th International Conference on Computer Science and Application Engineering, CSAE 2021 - Virtual, Online, China
Duration: 19 Oct 202121 Oct 2021

Publication series

NameACM International Conference Proceeding Series

Conference

Conference5th International Conference on Computer Science and Application Engineering, CSAE 2021
Country/TerritoryChina
CityVirtual, Online
Period19/10/2121/10/21

Keywords

  • Adaptive control
  • Evtol
  • Flexible frame
  • Input error

Fingerprint

Dive into the research topics of 'Flight Attitude Control of an Electric Vertical Takeoff and Landing with Flexible Frame'. Together they form a unique fingerprint.

Cite this