Fuzzy Roll Control System for Unmanned Aerial vehicle.

Nair, Vishnu G and Thakur, Mayank and George, V I and Dileep, M V (2012) Fuzzy Roll Control System for Unmanned Aerial vehicle. In: Proceedings of IX Control Instrumentation System Conference , 16-17 November 2012, Manipal.

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Abstract

When Designing a UAV , there are a tremendous amount of issues that a design team needs to be concerned with . Among a wide variety of other other important factors, an UAV’s stability and control is a key design parameter that must be met . Often times a UAV can be designed in such a way as to be inherently stable. That is a perturbation in the lateral or longitudinal dynamics of the UAV will not cause undesired effects; rather, the perturbation will be quickly damped out by the natural dynamics of the UAV . However often times other issues will call for an UAV to be designed with inherently unstable dynamics. High speed high performance fighter jets often fall in to this category. Stability is still necessary though, Because the natural dynamics of the system is unstable, automatic control must be used in order to bring about stability for the system. This paper describes one such unstable system, and describes fuzzy logic controller design that will satisfy performance specifications for the system.

Item Type: Conference or Workshop Item (Paper)
Uncontrolled Keywords: lib.mit@manipal.edu
Subjects: Engineering > MIT Manipal > Aeronautical and Automobile
Engineering > MIT Manipal > Instrumentation and Control
Depositing User: MIT Library
Date Deposited: 19 May 2015 11:26
Last Modified: 19 May 2015 11:26
URI: http://eprints.manipal.edu/id/eprint/142683

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