AIAA Modeling and Simulation Technologies Conference 2015
DOI: 10.2514/6.2015-2499
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Control validation of a morphing wing in an open loop architecture

Abstract: Aircraft wings are generally designed and optimized to give the best possible performance for cruise flight conditions. Using conventional control surfaces such as flaps, ailerons, variable wing sweep and spoilers, the structure of aircraft wings is changed for other flight conditions. With the introduction of wing morphing, the flow over an aircraft's wings can be modified locally to improve the overall wing and aircraft performance during the different flight steps. The goal of this research work is to devel… Show more

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Cited by 5 publications
(1 citation statement)
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“…28 In an experimental validated approach for the morphing wing control system, the implemented controller was compiled in C language and loaded inside the real time hardware system used in this project. 34,35 The input/output variables of the controller were configured and mapped carefully, according to the project requirements, its good working being proved experimentally, through bench testing and wind tunnel testing.…”
Section: A General Description Of Morphing Wing Projectmentioning
confidence: 99%
“…28 In an experimental validated approach for the morphing wing control system, the implemented controller was compiled in C language and loaded inside the real time hardware system used in this project. 34,35 The input/output variables of the controller were configured and mapped carefully, according to the project requirements, its good working being proved experimentally, through bench testing and wind tunnel testing.…”
Section: A General Description Of Morphing Wing Projectmentioning
confidence: 99%