Kinematic synthesis of flight control systems for light aircrafts

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Atıf İçin Kopyala

Yaman Y., Akman Y., Soylemez E.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.74, sa.1, ss.12-18, 2002 (SCI-Expanded)

• Yayın Türü: Makale / Tam Makale
• Cilt numarası: 74 Sayı: 1
• Basım Tarihi: 2002
• Doi Numarası: 10.1108/00022660210414985
• Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
• Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
• Sayfa Sayıları: ss.12-18
• Orta Doğu Teknik Üniversitesi Adresli: Evet

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.