Share Email Print
cover

Proceedings Paper

Structural analysis and aeroservoelastic response simulation of smart fin operated by piezoelectric actuators
Author(s): Chul-Woo Park; Byeong Uk Im; Yoo-Jin Kang; Kwang Joon Yoon; Bum Soo Yoon; SangJoon Shin
Format Member Price Non-Member Price
PDF $14.40 $18.00

Paper Abstract

In order to substitute a conventional fin operated by hydraulic actuators, a smart fin actuated by piezoelectric material was attempted. A straight unimorph actuator was embedded along the spanwise direction in the hollow inner space of the fin. A hinge which was constrained except the axial rotation was located at the 1/4th chord line, and this enabled the smart fin to rotate in its rigid pitch direction. In this paper, starting from the fundamental structural analysis, the aeroelastic and aeroservoelastic stability, and structural response simulations of the smart fin control system were performed by integration of MSC.NASTRAN, ZAERO and MATLAB/Simulink. The controller was designed to ensure the flight stability and to maintain the pitch angles of the smart fin under specific flight conditions. Closed-loop control system of the smart fin was constructed and analyzed by MATLAB/Simulink.

Paper Details

Date Published: 12 April 2017
PDF: 13 pages
Proc. SPIE 10168, Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2017, 101681C (12 April 2017); doi: 10.1117/12.2258359
Show Author Affiliations
Chul-Woo Park, LIG Nex1 Co., Ltd. (Korea, Republic of)
Byeong Uk Im, Seoul National Univ. (Korea, Republic of)
Yoo-Jin Kang, Korea Aerospace Insdustries, Ltd. (Korea, Republic of)
Kwang Joon Yoon, Konkuk Univ. (Korea, Republic of)
Bum Soo Yoon, Konkuk Univ. (Korea, Republic of)
SangJoon Shin, Seoul National Univ. (Korea, Republic of)


Published in SPIE Proceedings Vol. 10168:
Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2017
Jerome P. Lynch, Editor(s)

© SPIE. Terms of Use
Back to Top