Flight Dynamics Modeling of Dual Thrust System Hybrid UAV

Aryandi Marta, Abdul Muis

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

Abstract

The dual thrust system hybrid UAV combines the hover capabilities of the quadcopter and the endurance capabilities of the fixed-wing types in one aircraft. Its main goal was to eliminate the needs for runway access in the takeoff and landing process. This concept was implemented in the LSU-02 NGLD VTOL design to enhance flight missions. In general, this type of UAV have three flight modes: hover flight mode, transition mode, and fixed-wing mode. The design of transition control from hover to cruise flight was a challenge in itself. This study described the stages of designed mathematical model of Hybrid UAVs flight dynamic and gives an overview of transition control strategy to handle unstable and nonlinearities of flight movement. From motor specification, the drag and torque coefficient were set to 2. 2times 10{-4} N/s{2} and 5.58times 10{-6} Nm/ s{2} respectively to completed the model.

Original languageEnglish
Title of host publicationAIMS 2021 - International Conference on Artificial Intelligence and Mechatronics Systems
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781665424820
DOIs
Publication statusPublished - 28 Apr 2021
Event2021 International Conference on Artificial Intelligence and Mechatronics Systems, AIMS 2021 - Virtual, Bandung, Indonesia
Duration: 28 Apr 202130 Apr 2021

Publication series

NameAIMS 2021 - International Conference on Artificial Intelligence and Mechatronics Systems

Conference

Conference2021 International Conference on Artificial Intelligence and Mechatronics Systems, AIMS 2021
Country/TerritoryIndonesia
CityVirtual, Bandung
Period28/04/2130/04/21

Keywords

  • fixed-wing
  • fixed-wing mode
  • hover mode
  • transition mode
  • VTOL

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