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