TY  - JOUR
AB  - 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.
VL  - 74
IS  - 1
SN  - 0002-2667
DO  - 10.1108/00022660210414985
UR  - https://doi.org/10.1108/00022660210414985
AU  - Yaman Yavuz
AU  - Akman Yunus
AU  - Söylemez Eres
PY  - 2002
Y1  - 2002/01/01
TI  - Kinematic synthesis of flight control systems for light aircrafts
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 12
EP  - 18
Y2  - 2024/04/25
ER  -