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- W2372882940 abstract "One of the important space technology researches is the study of large-diameter high-precision satellite antenna structure,and the large loop satellite antenna is one of the key studies of the large-diameter high-precision satellite antenna structure.The large loop satellite antenna has the characteristics of large-size,big-flexible,low-stiffness,light-weight,weak-damping and low-natural frequency.With the increasing of antenna diameter,the low-order frequency of the large loop satellite antenna will located in the frequency range of satellite attitude adjustment,then the low-frequency,large-amplitude and long-time coupled vibration will be occurred during the adjustment process,it will affect the accuracy of the antenna and the process of orbital transfer.So we have to study the method to suppress the coupling vibration happening during the satellite attitude adjustment.Because of the limitation of spacecraft launch load,traditional methods such as design of enhancing the stiffness of satellite and antenna can't meet the requirements.The control capacity of traditional passive vibration control can't meet the requirements,either.On the background mentioned above,this paper studied active control of vibration of flexible loop antenna structure using a new PZT actuators,and performed further discussions and experiment study for them." @default.
- W2372882940 created "2016-06-24" @default.
- W2372882940 creator A5011640789 @default.
- W2372882940 date "2013-01-01" @default.
- W2372882940 modified "2023-09-26" @default.
- W2372882940 title "A piezoelectric actuator's application to active control of vibration of flexible loop antenna structure" @default.
- W2372882940 hasPublicationYear "2013" @default.
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