AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
PDF (1.5 MB)
Collect
Submit Manuscript AI Chat Paper
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Publishing Language: Chinese

An adaptive improved PD controller for rigid-elastic coupled launch vehicles

Xingyu JIANG1Fengfeng XUE2Fanghua JIANG2Peng SHI1Shengping GONG1( )
School of Astronautics,Beihang University,Beijing 100191,China
School of Aerospace Engineering,Tsinghua University,Beijing 100084,China
Show Author Information

Abstract

An improved proportional-derivative (PD) controller with adaptive capability is designed for the rigid-elastic coupled launch vehicle, aiming to achieve high-quality tracking of guidance instructions. The controller introduces an adaptive augmenting control (AAC) module, enhancing its parameter adjustment capabilities so that it can adaptively adjust both proportional and derivative coefficients simultaneously. Furthermore, an adaptive filter module is incorporated, with amplitude reduction complementing phase lag in the amplitude-phase characteristics of the transfer function. This filter adjusts its filtering effect adaptively based on the identification results of the elastic frequency. When applied to the pitch angle rate feedback channel, this filter effectively stabilizes the phase angle of the first-order elastic mode and the amplitude of the higher-order elastic mode. Numerical simulation results demonstrate that the designed adaptive improved PD controller not only has a simple structure and is easy to select parameters, but also exhibits excellent adaptive capabilities and significant elastic vibration suppression effects. Its remarkable engineering application value is demonstrated by its suitability for time-varying systems and its capacity to preserve system stability even in the presence of large model parameter variations.

CLC number: V448.1 Document code: A Article ID: 1001-5965(2026)07-2477-10

References

【1】
【1】
 
 
Journal of Beijing University of Aeronautics and Astronautics
Pages 2477-2486

{{item.num}}

Comments on this article

Go to comment

< Back to all reports

Review Status: {{reviewData.commendedNum}} Commended , {{reviewData.revisionRequiredNum}} Revision Required , {{reviewData.notCommendedNum}} Not Commended Under Peer Review

Review Comment

Close
Close
Cite this article:
JIANG X, XUE F, JIANG F, et al. An adaptive improved PD controller for rigid-elastic coupled launch vehicles. Journal of Beijing University of Aeronautics and Astronautics, 2026, 52(7): 2477-2486. https://doi.org/10.13700/j.bh.1001-5965.2024.0383

1

Views

0

Downloads

0

Crossref

0

Scopus

0

CSCD

Received: 04 June 2024
Published: 22 July 2024
© Journal of Beijing University of Aeronautics and Astronautics