Sliding mode control for a quad rotor unmanned aerial vehicle
Joint Authors
Gherouat, O.
Matuq, D.
Husam, A.
Abd al-Samad, F.
Source
Journal of Automation and Systems Engineering
Issue
Vol. 10, Issue 3 (30 Sep. 2016), pp.150-157, 8 p.
Publisher
Publication Date
2016-09-30
Country of Publication
Algeria
No. of Pages
8
Main Subjects
Engineering & Technology Sciences (Multidisciplinary)
Abstract EN
In this article the sliding mode controller is applied for a small unmanned helicopter called quadrotor.
The dynamic model is established considering various physical phenomena that can influence its dynamic behavior.
Subsequently, backstepping controller is designed.
Its job is to generate commands to the four rotors.
The objective is to drive the quadrotor to track desired Cartesians positions and desired orientation.
The proposed controller is based on the Lyapunov stability.
This control technique was checked in simulation and has given good performance.
American Psychological Association (APA)
Gherouat, O.& Matuq, D.& Husam, A.& Abd al-Samad, F.. 2016. Sliding mode control for a quad rotor unmanned aerial vehicle. Journal of Automation and Systems Engineering،Vol. 10, no. 3, pp.150-157.
https://search.emarefa.net/detail/BIM-754757
Modern Language Association (MLA)
Husam, A.…[et al.]. Sliding mode control for a quad rotor unmanned aerial vehicle. Journal of Automation and Systems Engineering Vol. 10, no. 3 (2016), pp.150-157.
https://search.emarefa.net/detail/BIM-754757
American Medical Association (AMA)
Gherouat, O.& Matuq, D.& Husam, A.& Abd al-Samad, F.. Sliding mode control for a quad rotor unmanned aerial vehicle. Journal of Automation and Systems Engineering. 2016. Vol. 10, no. 3, pp.150-157.
https://search.emarefa.net/detail/BIM-754757
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references : p. 157
Record ID
BIM-754757