框架面板式卫星在轨微振动仿真分析

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，¹，'，²，（1.2.）

关键词：框架面板式卫星；微振动；动量轮；帆板驱动；柔性多体系统动力学 中图分类号：0313.7 文献标志码：A DOI:10.16385/j.cnki.issn.1004-4523.202402001

Micro-vibration simulation analysis of a frame-panel satellite on orbit

CAI Zhengzheng', SUN Jialiang', JINDongping',CHEN Hongcheng², GUAN Shujun² (1.State Key Laboratory of Mechanics and Control for Aerospace Structures，Colege of Aerospace Engineering

NanjingUniversity ofAeronauticsand Astronautics，Nanjing21oo16，China;

2.Innovation Academy forMicrosatellites ofChinese Academy of Science，Shanghai 201203，China)

Abstract;Duringtheoobitoperationofasatelit，micro-vbratiosgneratedbyriousdisturbancesouessuchasmometuwheels andsolararaydriveseblies(ADA)ecttesatelitstiudstabityndpotingacracytrebyduingthpefancf sensitivepayloadsonboardBasedonthfxibleulti-bodydyamicsmodel,thispaperompreensivelyconsiderstheifueneofan disturbanceoucndondtsadacsuatdneobitmivbatioharacterstisofmpaeatelitUsinte absoluteodaloatefladttualodatefottitelitdsieaeeed; therigid-bodydyamic modelofthemomentm wheelisdrivedbasedontheLagrangeequation,andteobitaldynamicequatiosofthe entiresateliabdefoiWittoedtelibs dynamicmodelisalidatedfroteeaspcts:ertialaractesticsodalaalysis,andorbitoerationles.Numericala resultsshowtattmageoftsatelittideanglesissicallostetwitteactualdata.Tsapealystevibaion responseofssiepdsdespodibatirsssonlrodingtreticalereefobt vibration suppression.

Keywords:frame-panelsatelite;micro-vibration; momentumwheel;solararrydriveassembly;flexible multiodysystemdyamics

近年来，随着深空探测、对地观测和星际测量等技术的发展，对航天器的姿态稳定性和指向精度提出了更高的要求[1-3]。（剩余23569字）