Adaptive Suppression Method for Elastic Vibrations in the Control System of Guided Rocket

This paper proposes a method for the autonomous identification of elastic frequency and adaptive suppression of elastic vibration based on a priori information, in response to the lower elastic frequency and large frequency uncertainty range of guided rockets. Firstly, this method uses fast Fourier...

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Bibliographic Details
Main Authors: Chen-ming Zheng, Cheng Zhang, Jun Wang, Zhang-yao Zheng
Format: Article
Language:English
Published: Wiley 2025-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/ijae/9348766
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