Kinematic synthesis of flight control systems for light aircrafts


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Yaman Y. , Akman Y., Soylemez E.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.74, ss.12-18, 2002 (SCI İndekslerine Giren Dergi) identifier identifier

  • Cilt numarası: 74 Konu: 1
  • Basım Tarihi: 2002
  • Doi Numarası: 10.1108/00022660210414985
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Sayfa Sayıları: ss.12-18

Özet

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.