In this paper, kinematic synthesis of a planar flight control system mechanism has been conducted for a light aircraft designed and built by TAI. 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.
Kinematic synthesis of flight control systems for light aircrafts
Aircraft Engineering and Aerospace Technology ; 74 , 1 ; 12-18
2002-02-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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