Transient Flight Controller of Vertical Take-Off and Landing UAV based on Multimode Integrated Design

Bin Wu, Xiaodong Song, Zhenchang Liu

Research output: Contribution to journalConference articlepeer-review

Abstract

the controller is designed for the vertical take-off and landing mode, the transient flight mode and the fixed wing flight mode, respectively; a control signal fusion method is introduced in the transition flight control mode, which realizes the smooth switching of aerial vehicle in different flight modes; aiming at the problem of the control plane redundancy, the method of advancing amplitude of redundant control quantity is adopted to simplify the control distribution process. It is verified that the control method of Vertical Take-Off and Landing UAV can track the flight path well via six degrees of freedom simulation of the aerial vehicle.

Original languageEnglish
Article number072068
JournalJournal of Physics: Conference Series
Volume1486
Issue number7
DOIs
Publication statusPublished - 17 Apr 2020
Event2019 4th International Seminar on Computer Technology, Mechanical and Electrical Engineering, ISCME 2019 - Chengdu, China
Duration: 13 Dec 201915 Dec 2019

Fingerprint

Dive into the research topics of 'Transient Flight Controller of Vertical Take-Off and Landing UAV based on Multimode Integrated Design'. Together they form a unique fingerprint.

Cite this