{"title":"轨道条件下电场强度控制的振动调制器","authors":"R.Yu. Dorofeev, D. Kozlov, I. Smirnov, A. Zhukov","doi":"10.17238/ISSN2409-0239.2016.3.84","DOIUrl":null,"url":null,"abstract":". The paper discusses the results of system research of the functioning peculiarities and characteristics of a vibration electric field modulator. Modulator output signal values in electric field with intensity in the range of 0 ∼ 250 kV/m are obtained. The following main metrological characteristics of a microsystem vibration modulator are identified: sensitivity, sensitivity threshold, response time, and static pattern. The modulator is classified depending on the method for producing an output signal from the input value on the nature of dependency of the output signal on the input signal, type of action, and scope of use. In conclusion it is determined that it is possible to use the developed product for electric field control on the spacecraft in orbital conditions.","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"115 19 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Vibration Modulator for Electric Field Intensity Control in Orbital Conditions\",\"authors\":\"R.Yu. Dorofeev, D. Kozlov, I. Smirnov, A. Zhukov\",\"doi\":\"10.17238/ISSN2409-0239.2016.3.84\",\"DOIUrl\":null,\"url\":null,\"abstract\":\". The paper discusses the results of system research of the functioning peculiarities and characteristics of a vibration electric field modulator. Modulator output signal values in electric field with intensity in the range of 0 ∼ 250 kV/m are obtained. The following main metrological characteristics of a microsystem vibration modulator are identified: sensitivity, sensitivity threshold, response time, and static pattern. The modulator is classified depending on the method for producing an output signal from the input value on the nature of dependency of the output signal on the input signal, type of action, and scope of use. In conclusion it is determined that it is possible to use the developed product for electric field control on the spacecraft in orbital conditions.\",\"PeriodicalId\":436954,\"journal\":{\"name\":\"Rocket-Space Device Engineering and Information Systems\",\"volume\":\"115 19 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Rocket-Space Device Engineering and Information Systems\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.17238/ISSN2409-0239.2016.3.84\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Rocket-Space Device Engineering and Information Systems","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.17238/ISSN2409-0239.2016.3.84","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Vibration Modulator for Electric Field Intensity Control in Orbital Conditions
. The paper discusses the results of system research of the functioning peculiarities and characteristics of a vibration electric field modulator. Modulator output signal values in electric field with intensity in the range of 0 ∼ 250 kV/m are obtained. The following main metrological characteristics of a microsystem vibration modulator are identified: sensitivity, sensitivity threshold, response time, and static pattern. The modulator is classified depending on the method for producing an output signal from the input value on the nature of dependency of the output signal on the input signal, type of action, and scope of use. In conclusion it is determined that it is possible to use the developed product for electric field control on the spacecraft in orbital conditions.
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