Transition flight modeling and robust control of a VTOL unmanned quad tilt-rotor aerial vehicle

Navya Thirumaleshwar Hegde, V. I. George, C. Gurudas Nayak, Kamlesh Kumar

Research output: Contribution to journalArticle

Abstract

The development of fully autonomous Unmanned Aerial Vehicles (UAV) plays a major contribution towards reducing the risk to human life in various applications including rescue teams, border patrol, police and inspection of buildings, pipelines, coasts, and terrains. Tiltrotor hybrid UAV exhibit special application value due to its unique rotor structure. The variation in the model dynamics and aerodynamics due to the tilting rotors are the major key issues and challenges which attracted the attention of many researchers. This vehicle combines the hovering capabilities of a helicopter along with the high-speed cruise capabilities of a conventional airplane by tilting its four rotors. In the present research work, the authors attempt to model a quad tilt rotor UAV using Newton-Euler formulation. A dynamic model of the vehicle is derived mathematically for horizontal, vertical and transition flight modes. A robust H-infinity control strategy is proposed, evaluated and analyzed through simulation to control the flight dynamics of the different modes of the UAV. Simulation results shows that the tiltrotor UAV achieves transition successfully.

Original languageEnglish
Pages (from-to)1252-1261
Number of pages10
JournalIndonesian Journal of Electrical Engineering and Computer Science
Volume18
Issue number3
DOIs
Publication statusPublished - 01-01-2020

Fingerprint

Robust control
Unmanned aerial vehicles (UAV)
Tilt
Robust Control
Rotor
Rotors
Antennas
Tilting
Modeling
Dynamic models
Flight Dynamics
Helicopter
Flight dynamics
Aerodynamics
Control Strategy
Euler
Inspection
Law enforcement
Dynamic Model
Simulation

All Science Journal Classification (ASJC) codes

  • Signal Processing
  • Information Systems
  • Hardware and Architecture
  • Computer Networks and Communications
  • Control and Optimization
  • Electrical and Electronic Engineering

Cite this

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Transition flight modeling and robust control of a VTOL unmanned quad tilt-rotor aerial vehicle. / Hegde, Navya Thirumaleshwar; George, V. I.; Gurudas Nayak, C.; Kumar, Kamlesh.

In: Indonesian Journal of Electrical Engineering and Computer Science, Vol. 18, No. 3, 01.01.2020, p. 1252-1261.

Research output: Contribution to journalArticle

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