Novel Active–Passive Piezoelectric Hybrid Constrained-Layer Damping Technique for Vibration Isolation in a Whole Spacecraft-Reference-Cited by-同舟云学术

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Novel Active–Passive Piezoelectric Hybrid Constrained-Layer Damping Technique for Vibration Isolation in a Whole Spacecraft

Published:2024-11 Issue:6 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Li Ming-Ming¹,Tang Ye²,Fang Bo³

Affiliation:

1. Dept. of System Design, China Satellite Network System Co. Ltd, HengYi Building, No. 5 Anding Rd., Chaoyang, Beijing 100029, China.

2. Associate Professor, Dept. of Mechanics, Tianjin Univ., Tianjin 300035, China; Ocean Institute, Northwestern Polytechnical Univ., Suzhou 215000, China (corresponding author).

3. Professor, School of Astronautics, Harbin Institute of Technology, Harbin 150001, China.

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5060

Reference41 articles.

1. Frequency equations for the in-plane vibration of circular annular disks;Bashmal S.;Adv. Acoust. Vib.,2010

2. Optimum Design and Control of Active Constrained Layer Damping

3. Attitude tracking control for reentry vehicles using centralised robust model predictive control

4. Dual-Loop Tube-Based Robust Model Predictive Attitude Tracking Control for Spacecraft With System Constraints and Additive Disturbances

5. Solving Constrained Trajectory Planning Problems Using Biased Particle Swarm Optimization

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