Design of self balancing pitch control in fixed wing unmanned aerial vehicle with fuzzy logic controller

Triwiyatno , Aris and Prakoso, Teguh and Amien S, Wahyul and Setiyono , Budi and Panggi Wijaya, Aristya Design of self balancing pitch control in fixed wing unmanned aerial vehicle with fuzzy logic controller. In: 2015 2nd International Conference on Information Technology, Computer, and Electrical Engineering (ICITACEE), 16-18 Oct. 2015, Semarang, Indonesia.

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Abstract

In UAV flight controller's design, the occurrence of errors due to the delay in the system response to the reference signal from the pilot and the lack of stability in flat conditions due to interference or unbalanced mechanical load. When this happens UAV can not be controlled and the flight conditions can not be maintained any more. Fuzzy controller offers a solution for the development of UAV's stability controllers, specialized in the design of the autopilot system that controls the pitch angle of the UAV. This research has been developing a prototype of fixed wing UAV that can be controlled wirelessly and has ability to maintain the balance on the pitch angle of the flat conditions (self-balancing). Run test results show that the applied fuzzy method succesfully controls the pitch angle to maintain a flat condition the developed UAV.

Item Type:Conference or Workshop Item (Paper)
Subjects:T Technology > T Technology (General)
Divisions:Faculty of Engineering > Department of Electrical Engineering
Faculty of Engineering > Department of Electrical Engineering
ID Code:77989
Deposited By:mahfudin mahfudin mahfudin
Deposited On:30 Oct 2019 13:26
Last Modified:14 Feb 2020 11:11

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