DocumentCode :
722935
Title :
Flexible membrane wing warping using tendon-sheath mechanism
Author :
Shian Lee ; Tjahjowidodo, Tegoeh ; Seung Ki Moon
Author_Institution :
Sch. of Mech. & Aerosp. Eng., Nanyang Technol. Univ., Singapore, Singapore
fYear :
2015
fDate :
16-19 June 2015
Firstpage :
624
Lastpage :
629
Abstract :
Flexible membrane wings have many advantages, but has very little roll control authority. In this paper, the flexible membrane wing is actuated using a tendon-sheath mechanism to achieve roll control and also allowing the wing to fold. The characteristics of the flexible wing, as well as the wing warping actuation approach is discussed in this paper. The experimental setup and results are shown. The characteristics of the tendon-sheath is shown to be suitable for flexible wing actuation. A simple nonlinear curve fitting model is also presented.
Keywords :
aerospace components; autonomous aerial vehicles; curve fitting; nonlinear control systems; UAV; flexible membrane wing warping; nonlinear curve fitting model; roll control; tendon-sheath mechanism; unmanned aerial vehicles; wing warping actuation approach; Aerodynamics; Force; Friction; Hysteresis; Servomotors; Shape; Tendons; Flexible membrane wing; hysteresis modeling; tendon-sheath mechanism; wing warping;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Automation (MED), 2015 23th Mediterranean Conference on
Conference_Location :
Torremolinos
Type :
conf
DOI :
10.1109/MED.2015.7158816
Filename :
7158816
Link To Document :
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