Kinematic synthesis of flight control systems for light aircrafts

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 ana...

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Bibliographic Details
Published inAIRCR ENG AEROSP TECHNOL Vol. 74; no. 1; pp. 12 - 18
Main Authors Yaman, Yavuz, Akman, Yunus, Söylemez, Eres
Format Journal Article
LanguageEnglish
Published Bradford MCB UP Ltd 01.01.2002
Emerald Group Publishing Limited
Subjects
Accuracy
Aerospace industry
Aircraft
Aviation
Control system synthesis
Control systems
Design
Error analysis
Experiments
Kinematics
Mathematical models
Structural analysis
Control systems
Aircraft
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Summary: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.
Bibliography:ObjectType-Article-2
SourceType-Scholarly Journals-1
ObjectType-Feature-1
content type line 23
ISSN:1748-8842
0002-2667
1758-4213
DOI:10.1108/00022660210414985