Proportional fuzzy feed-forward architecture control validation by wind tunnel tests of a morphing wing
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DOI: 10.1016/j.cja.2017.02.001
Abstract: Abstract In aircraft wing design, engineers aim to provide the best possible aerodynamic performance under cruise flight conditions in terms of lift-to-drag ratio. Conventional control surfaces such as flaps, ailerons, variable wing sweep and spoilers… read more here.
Keywords: aircraft; control; proportional fuzzy; flight ... See more keywords