Vibration-attitude integrated control of a large two-dimensional planar phased array antenna

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2025-02-07 DOI:10.1016/j.ast.2025.110030
Li Pei , Liu Xiang , Cai Guoping , Sun Jun , Zhu Dongfang
{"title":"Vibration-attitude integrated control of a large two-dimensional planar phased array antenna","authors":"Li Pei ,&nbsp;Liu Xiang ,&nbsp;Cai Guoping ,&nbsp;Sun Jun ,&nbsp;Zhu Dongfang","doi":"10.1016/j.ast.2025.110030","DOIUrl":null,"url":null,"abstract":"<div><div>Phased array antennas are pivotal for observing, identifying, and tracking targets, serving both military and civilian needs. They are growing larger and more complex to meet the demand for high-resolution Earth observation. However, their intricate design, low-frequency density, and significant coupling make dynamic analysis and control design challenging. This paper introduces a novel large-scale, space-deployable, two-dimensional planar phased array antenna and investigates its dynamic modeling and active control. Unlike traditional one-dimensional phased array antenna, this antenna can scan in two directions, providing a larger scanning area. To suppress antenna vibration, the paper proposes a control strategy using ropes as actuators. Firstly, the paper details the structure of the phased array antenna, including its attitude and vibration actuators. Then, using the hybrid coordinate method and the velocity variation principle, it derives the antenna's rigid-flexible coupled dynamic model. Subsequently, the paper designs an attitude-vibration controller for the antenna, integrating the computed torque control method, Linear Quadratic Regulator (LQR), and Bang-Bang control theory. This includes considering the unidirectionality and saturation of the rope control forces and optimizing the placement of rope actuators using Particle Swarm Optimization (PSO). Finally, numerical simulations validate the effectiveness and accuracy of the theoretical investigation. The results indicate that the antenna model possesses characteristics of low-frequency density and robust rigidity-flexibility coupling, with optimization of actuator quantity and placement enhancing control efficiency. Furthermore, the dynamic model accurately describes the antenna's behavior, achieving results consistent with ADAMS software. The attitude-vibration coupled controller maintains precise directional accuracy, effectively suppressing vibrations.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"160 ","pages":"Article 110030"},"PeriodicalIF":5.0000,"publicationDate":"2025-02-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963825000975","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

Phased array antennas are pivotal for observing, identifying, and tracking targets, serving both military and civilian needs. They are growing larger and more complex to meet the demand for high-resolution Earth observation. However, their intricate design, low-frequency density, and significant coupling make dynamic analysis and control design challenging. This paper introduces a novel large-scale, space-deployable, two-dimensional planar phased array antenna and investigates its dynamic modeling and active control. Unlike traditional one-dimensional phased array antenna, this antenna can scan in two directions, providing a larger scanning area. To suppress antenna vibration, the paper proposes a control strategy using ropes as actuators. Firstly, the paper details the structure of the phased array antenna, including its attitude and vibration actuators. Then, using the hybrid coordinate method and the velocity variation principle, it derives the antenna's rigid-flexible coupled dynamic model. Subsequently, the paper designs an attitude-vibration controller for the antenna, integrating the computed torque control method, Linear Quadratic Regulator (LQR), and Bang-Bang control theory. This includes considering the unidirectionality and saturation of the rope control forces and optimizing the placement of rope actuators using Particle Swarm Optimization (PSO). Finally, numerical simulations validate the effectiveness and accuracy of the theoretical investigation. The results indicate that the antenna model possesses characteristics of low-frequency density and robust rigidity-flexibility coupling, with optimization of actuator quantity and placement enhancing control efficiency. Furthermore, the dynamic model accurately describes the antenna's behavior, achieving results consistent with ADAMS software. The attitude-vibration coupled controller maintains precise directional accuracy, effectively suppressing vibrations.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
求助全文
约1分钟内获得全文 去求助
来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
期刊最新文献
Aerothermal performance of different relative positions of holes and ribs of a flat-plate film cooling hole with a straight-ribbed crossflow coolant channel Numerical investigation of the velocity-coupled response of propellant burning rate in a solid rocket motor Physical investigation on the sound transmission loss of heterogeneous metastructures using wave-based methodologies Aeroacoustics evaluation and mechanism of Krueger flap An intelligent prediction method for supersonic flow field in scramjet isolator enhanced by feature details
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1