Cited By
View all- Musoles JGarcia-Nieto SSimarro RRamos C(2024)Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2Electronics10.3390/electronics1313249713:13(2497)Online publication date: 26-Jun-2024
Tri-Tilting Rotor Fixed-Wing VTOL UAV: Dynamic Modelling and Transition Flight Control
Pages 66 - 71
Abstract
This paper gives the dynamic modeling and design of a controller for autonomous Vertical take-off and landing (VTOL) Tri-Tilt rotor hybrid Unmanned Aerial Vehicle (UAV). Nowadays, UAVs have experienced remarkable progress and mainly categorized into fixed-wing UAVs and rotary-wing UAVs. The Tri Tiltrotor UAV models are derived mathematically using Euler's force and moment equations for VTOL to horizontal flight and vice-versa using MATLAB. The development of fully autonomous and self-guided UAVs would reduce the risk to human life. The applications consist of inspection of coasts, terrain, border, patrol buildings, rescue teams, police, and pipelines. A Proportional-Integral-Derivative control method is proposed for UAVs attitude and altitude stabilization. The results reveal that the controller accomplishes adaptability, robust performance and stability in the transition mode.
References
[1]
P. Castillo, R. Lozano, and A. Dzul, “Modelling and control of mini-flying machines,” Springer-Verlag in Advances in Industrial Control, ISBN: 1-85233-957-8, (2005)
[2]
Miller, M. and Narkiewicz, J. Tiltrotor modelling for simulation in various flight conditions. Journal of theoretical and applied mechanics, 44(4):881-906, (2006).
[3]
Flores, G. R., Escareno, J., Lozano, R., and Salazar, S. Quad-tilting rotor convertible mav: Modeling and real-time hover flight control. Journal of Intelligent & Robotic Systems, 65(1-4):457-471, (2012)
[4]
Kada, B. and Ghazzawi, Y. Robust PID controller design for an UAV flight control system. Proceedings of the World Congress on Engineering and Computer Science 2 (1-6) (2011).
[5]
Aedo, O., Barbosa, K.A. and Álvarez, A. Mixed controller design for an UAV flight control system. IEEE Chilean Conference on Electrical, Electronics Engineering, Information and Communication Technologies (CHILECON), 135-140, (2015)
[6]
Kaan Taha ¨Oner, Ertu Grul C¸ Et insoy, Efe Sirimoglu, Cevdet Hanc¸ER, “Mathematical modelling and vertical flight control of a tilt-wing UAV”, Turkish Journal Of Electrical Engineering & Computer Sciences, (2012).
[7]
Andrew Zulu, Samuel John, “A Review of Control Algorithms for Autonomous Quadrotors”, Open Journal of Applied Sciences, 2014, 4, 547-556 Published Online December in SciRes, (2014).
[8]
Chen, C., Zhang, J., Zhang, D., and Shen, L. Control and flight test of a tiltrotor unmanned aerial vehicle. International Journal of Advanced Robotic Systems, 14(1), (2017).
[9]
Yuksek, B., Vuruskan, A., Ozdemir, U., Yukselen, M., and Inalhan, G. Transition flight modeling of a fixed-wing vtol uav. Journal of Intelligent & Robotic Systems, 84(1-4):83-105, (2016).
[10]
Ben Khoud, K. and Bouall_egue, S. (2016). Modeling and lqg controller design for a quad tilt-wing uav. In Proceedings of the 3rd international conference on automation, control engineering and computer science (ACECS2016), Hammamet, March, pages 20-22.
Index Terms
- Tri-Tilting Rotor Fixed-Wing VTOL UAV: Dynamic Modelling and Transition Flight Control
Index terms have been assigned to the content through auto-classification.
Recommendations
Transition Flight Modeling of a Fixed-Wing VTOL UAV
This paper describes a complete six-degree-of-freedom nonlinear mathematical model of a tilt rotor unmanned aerial vehicle (UAV). The model is specifically tailored for the design of a hover to forward flight and forward flight to hover transition ...
Automatic Control for Aerobatic Maneuvering of Agile Fixed-Wing UAVs
The use of unmanned aerial vehicles (UAVs) has become ubiquitous in a broadening range of applications, including many civilian uses. UAVs are typically categorized into two categories: conventional fixed-wing aircraft, which are associated with ...
Optimal transition from hovering to level-flight of a quadrotor tail-sitter UAV
A quadrotor equipped with a fixed-wing (hereinafter referred to as the quadrotor tail-sitter UAV) has been developed by authors. The quadrotor tail-sitter UAV can hover like a quadrotor and can fly like a fixed-wing airplane. The remarkable ...
Comments
Information & Contributors
Information
Published In
February 2021
644 pages
ISBN:9781450389839
DOI:10.1145/3459104
Copyright © 2021 ACM.
Permission to make digital or hard copies of all or part of this work for personal or classroom use is granted without fee provided that copies are not made or distributed for profit or commercial advantage and that copies bear this notice and the full citation on the first page. Copyrights for components of this work owned by others than ACM must be honored. Abstracting with credit is permitted. To copy otherwise, or republish, to post on servers or to redistribute to lists, requires prior specific permission and/or a fee. Request permissions from [email protected]
Publisher
Association for Computing Machinery
New York, NY, United States
Publication History
Published: 20 July 2021
Check for updates
Qualifiers
- Research-article
- Research
- Refereed limited
Conference
ISEEIE 2021
ISEEIE 2021: 2021 International Symposium on Electrical, Electronics and Information Engineering
February 19 - 21, 2021
Seoul, Republic of Korea
Contributors
Other Metrics
Bibliometrics & Citations
Bibliometrics
Article Metrics
- View Citations1Total Citations
- 200Total Downloads
- Downloads (Last 12 months)33
- Downloads (Last 6 weeks)3
Reflects downloads up to 25 Dec 2024
Other Metrics
Citations
Cited By
View all- Musoles JGarcia-Nieto SSimarro RRamos C(2024)Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2Electronics10.3390/electronics1313249713:13(2497)Online publication date: 26-Jun-2024
View Options
Login options
Check if you have access through your login credentials or your institution to get full access on this article.
Sign inFull Access
View options
View or Download as a PDF file.
PDFeReader
View online with eReader.
eReaderHTML Format
View this article in HTML Format.
HTML Format