Kadmiry, Bourhane Driankov, D. 2004 (English)In: IEEE transactions on fuzzy systems, ISSN 1063-6706, E-ISSN 1941-0034, Vol. 12, no 4, 502-515Article in journal (Refereed) Published
In this paper, we address the design of an attitude controller that achieves stable, and robust aggressive maneuverability for an unmanned helicopter. The controller proposed is in the form of a fuzzy gain-scheduler, and is used for stable and robust altitude, roll, pitch, and yaw control. The controller is obtained from a realistic nonlinear multiple-input-multiple-output model of a real unmanned helicopter platform, the APID-MK3. The results of this work are illustrated by extensive simulation, showing that the objective of aggressive, and robust maneuverability has been achieved. © 2004 IEEE.
unmanned helicopter, Takagi-Sugeno fuzzy control, fuzzy gain scheduling, output-feedback fuzzy control
National CategoryEngineering and Technology
Identifiersurn:nbn:se:liu:diva-45682 (URN)10.1109/TFUZZ.2004.832539 (DOI)oai:DiVA.org:liu-45682 (OAI)diva2:266578 (DiVA)