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.
Yaman, Y., Akman, Y. and Söylemez, E. (2002), "Kinematic synthesis of flight control systems for light aircrafts", Aircraft Engineering and Aerospace Technology, Vol. 74 No. 1, pp. 12-18. https://doi.org/10.1108/00022660210414985Download as .RIS
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