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Kinematic synthesis of flight control systems for light aircrafts

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2002-01-01
Yaman, Yavuz
Akman, Y
Soylemez, E
In this paper, kinematic synthesis of a planar flight control system mechanism has been conducted for a light aircraft designed and built by TAL To achieve a simple construction, the four-bar linkages are used in the synthesis. Freudenstein's Method and Bloch's Method are utilized for analytical three and four bar position syntheses respectively. A case study of an elevator flight control system is presented.