Kinematic synthesis of flight control systems for light aircrafts

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2002-01-01

Author

Yaman, Yavuz
Soylemez, E

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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.

Subject Keywords

Control systems, Aircraft

URI

https://hdl.handle.net/11511/41049

Journal

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY

DOI

https://doi.org/10.1108/00022660210414985

Collections

Department of Aerospace Engineering, Article

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Citation Formats

Y. Yaman and E. Soylemez, “Kinematic synthesis of flight control systems for light aircrafts,” AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, pp. 12–18, 2002, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/41049.