Structure-Actuator Integrated Design of Piezo-Actuated Composite Plate Wing for Active Shape Control-Reference-Cited by-同舟云学术

Structure-Actuator Integrated Design of Piezo-Actuated Composite Plate Wing for Active Shape Control

Published:2021-11 Issue:6 Volume:34 Page:04021070
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhou Wenya¹^ORCID,Zhang Zongyu²,Wang Xiaoming³,Lv Weiliang⁴,Hu Xinhan⁵

Affiliation:

1. Associate Professor, School of Aeronautics and Astronautics, Liaoning Provincial Key Laboratory of Aerospace Advanced Technology, Dalian Univ. of Technology, Dalian 116024, China. ORCID: .

2. Doctoral Student, School of Aeronautics and Astronautics, Sun Yat-sen Univ., Guangzhou 510006, China.

3. Associate Professor, School of Mechanical and Electrical Engineering, Guangzhou Univ., Guangzhou 510006, China (corresponding author).

4. Associate Professor, School of Aeronautics and Astronautics, Dalian Univ. of Technology, Dalian 116024, China.

5. Graduate Student, School of Aeronautics and Astronautics, Dalian Univ. of Technology, Dalian 116024, China.

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.1943-5525.0001322

Reference62 articles.

1. Finite element method for piezoelectric vibration

2. Design optimization of composite laminated structures using genetic algorithms and finite element analysis

3. Tuning of PID controller based on a multiobjective genetic algorithm applied to a robotic manipulator

4. A Review of Morphing Aircraft

5. Anisotropic Actuation with Piezoelectric Fiber Composites

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A Review: Structural Shape and Stress Control Techniques and their Applications;Archives of Computational Methods in Engineering;2024-06-26

2. Active shape control for flexible space structures using an optimal gyricity distribution;Advances in Space Research;2023-01