L1 Adaptive Control of a Projectile Fin by Piezoelectric Actuator-Reference-Cited by-同舟云学术

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L1 Adaptive Control of a Projectile Fin by Piezoelectric Actuator

Published:2014-07 Issue:4 Volume:27 Page:06014002
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Lee Keum W.¹,Singh Sahjendra N.²

Affiliation:

1. Professor, Division of Electronic Information and Communication, Univ. of Kwandong, Gangwon 210-701, South Korea.

2. Professor, Dept. of Electrical and Computer Engineering, Univ. of Nevada Las Vegas, Las Vegas, NV 89154-4026 (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000288

Reference30 articles.

1. Distributed piezoelectric-polymer active vibration control of a cantilever beam

2. Active plate and missile wing development using directionally attached piezoelectric elements;Barrett R.;J. Guid. Contr. Dyn.,1994

3. Missile flight control using active flexspar actuators

4. Enhancement of the dynamic buckling load for a plate by using piezoceramic actuators

5. Deflection control during dynamic deformations of a rectangular plate using piezoceramic elements

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