Hybrid-Powered Tri-Quadrotor with Main and Secondary Rotors

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

Abstract

To address the issues of limited endurance and low payload capacity in electric UAVs, this paper proposes a novel parallel hybrid-powered quadrotor design. The design features a configuration that combines a main rotor and secondary rotors, with the main rotor driven by an internal combustion engine to provide the primary lift. The secondary rotors, driven by electric motors and tilted at a 3D-degree angle, are responsible for adjusting the UAV's attitude. This paper develops dynamic models for both the engine and the UAV, and designs corresponding control algorithms. Through simulation validation, the proposed control algorithms have been shown to effectively ensure the stable flight of the UAV. The parallel hybrid power system fully leverages the high energy density of fuel, significantly enhancing the UAV's endurance and payload capacity.

Original languageEnglish
Title of host publicationProceedings of the 37th Chinese Control and Decision Conference, CCDC 2025
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages6401-6406
Number of pages6
ISBN (Electronic)9798331510565
DOIs
Publication statusPublished - 2025
Externally publishedYes
Event37th Chinese Control and Decision Conference, CCDC 2025 - Xiamen, China
Duration: 16 May 202519 May 2025

Publication series

NameProceedings of the 37th Chinese Control and Decision Conference, CCDC 2025

Conference

Conference37th Chinese Control and Decision Conference, CCDC 2025
Country/TerritoryChina
CityXiamen
Period16/05/2519/05/25

Keywords

  • control allocation
  • parallel hybrid power
  • tri-quadrotor
  • unmanned aerial vehicle (UAV)

Fingerprint

Dive into the research topics of 'Hybrid-Powered Tri-Quadrotor with Main and Secondary Rotors'. Together they form a unique fingerprint.

Cite this