Novel approach for active vibration control of a flexible missile-Reference-Cited by-同舟云学术

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Novel approach for active vibration control of a flexible missile

Published:2020-08 Issue:4 Volume:16 Page:956-967
ISSN:2214-9147
Container-title:Defence Technology
language:en
Short-container-title:Defence Technology

Author:

Pan Cheng-long,Rong Ji-li,Xu Tian-fu,Xiang Da-lin

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Metals and Alloys,Mechanical Engineering,Ceramics and Composites,Computational Mechanics

Reference49 articles.

1. Dynamic stability of flexible missile under constant and pulsating thrusts;Beal;AIAA J,1965

2. Aeroelastic stability of slender, spinning missiles;Platus;J Guid Control Dyn,1992

3. Effect of thrust on aeroelastic stability of a slender missile;Xu,2008

4. Aeroelastic stability of a slender missile with constant thrust;Wu;Procedia Eng,2012

5. Elastic dynamic effects on the trajectory of a flexible launch vehicle;Li;J Spacecr Rocket,2015

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1. Research on Missile Vibration Characteristics Considering Engine Vibration Based on Mstmm;Lecture Notes in Mechanical Engineering;2024

2. Flight Performance and Dispersion Analysis for a Flexible Tactical Missile;Journal of Spacecraft and Rockets;2023-07

3. Active vibration control for three-dimensional braided composite beams based on piezoelectric sensor and actuator;Journal of Mechanics of Materials and Structures;2023-05-30

4. Mini-max optimization of actuator/sensor placement for flexural vibration control of a rotating thin-walled cylinder over a range of speeds;Journal of Sound and Vibration;2021-08

5. Limitations of autopilot design for controlling a statically unstable flexible interceptor;Journal of the Franklin Institute;2021-08

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