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作 者:Weida XING Weixiao TUO Xingfei LI Tianyu WANG Chenxi YANG
机构地区:[1]State Key Laboratory of Precision Measurement Technology and Instruments,Tianjin University,Tianjin 30072,China [2]Taihu Laboratory of Deepsea Technological Science,Wuxi 214123,China
出 处:《Chinese Journal of Aeronautics》2024年第9期1-19,共19页中国航空学报(英文版)
基 金:supported by the National Natural Science Foundation of China (No.62203322);the China Postdoctoral Science Foundation (No.2022M712372);the Enlisting and Leading Program of the Taihu Laboratory of Deepsea Technological Science,China (No.2022JBGS03001).
摘 要:Micro-vibration is an important factor affecting the imaging quality and pointing accu-racy of the in-orbit satellites.To address the problem of micro-vibration compensation,a general summary for modeling,analysis,suppression,and compensation approach should be outlined.In this review,micro-vibration characteristics and its impacts on the payloads are firstly analyzed.Afterwards,methods for micro-vibration measurement are provided.In detail,the principles and practical applications of these methods are introduced.Then,advanced technologies for micro-vibration suppression are summarized from micro-vibration source attenuation,transfer path opti-mization and sensitive load isolation.Two approaches have been found to be effective for micro-vibration compensation.The one is the Line-of-Sight(LOS)stabilization assisted with Inertial Ref-erence Unit(IRU).The other is using image restoration technology to remove the blur caused by platform jitter.The compensation technique and research status of the two techniques are reviewed.This work will provide researchers with technical guidelines for micro-vibration suppression.
关 键 词:In-orbit Satellite Micro-vibration suppression Compensation technique Vibration isolation Path optimization
分 类 号:V414[航空宇航科学与技术—航空宇航推进理论与工程]
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