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contributor authorAli Reza Babaei
contributor authorMahdi Mortazavi
contributor authorMohammad Hassan Moradi
date accessioned2017-05-08T21:33:50Z
date available2017-05-08T21:33:50Z
date copyrightJanuary 2012
date issued2012
identifier other%28asce%29as%2E1943-5525%2E0000116.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56260
description abstractIn this paper, the authors tried to design the altitude hold mode autopilot for unmanned aerial vehicles. This case presents an interesting challenge attributable to the nonminimum phase characteristic, nonlinearities, and uncertainties of the altitude to elevator relationship. A fuzzy logic autopilot in a single-loop scheme is proposed for the design of this autopilot. The multiobjective genetic algorithm is used to mechanize the optimal determination of fuzzy logic autopilot parameters on the basis of an efficient cost function that comprises undershoot, overshoot, rise time, settling time, steady state error, and stability. Simulation results show that the proposed strategy not only has a simple structure, but also has desirable performances in time response characteristics, robustness (against the unmodeled nonlinear terms and parametric uncertainties), and the adaptation of itself than the large commands.
publisherAmerican Society of Civil Engineers
titleFuzzy-Genetic Autopilot Design for Nonminimum Phase and Nonlinear Unmanned Aerial Vehicles
typeJournal Paper
journal volume25
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000116
treeJournal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 001
contenttypeFulltext


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