{"title":"蜗壳天线性能的理论设计与预测","authors":"H.S.C. Wang","doi":"10.1109/AERO.1990.109093","DOIUrl":null,"url":null,"abstract":"To provide generic design guidelines for volute antenna elements over a wide range of parameters, a theoretical formulation and algorithm for computing the antenna radiation field have been developed. From these computed field values, the antenna directivity, 3-dB beamwidth, axial ratio, and front/back ratio can be evaluated for the purpose of design tradeoff considerations. The technical approach used is to compute the radiation fields for the helical wires and the straight-end connecting wires, based on a sinusoidal current distribution model along each of the four filaments or wires of the volute. Using axial length as a running variable, a complete tradeoff for the case of the half-turn, half-wavelength volute to meet certain special requirements was considered as an example for design analysis.<<ETX>>","PeriodicalId":141316,"journal":{"name":"IEEE Conference on Aerospace Applications","volume":"31 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1990-02-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Theoretical design and predictions of volute antenna performance\",\"authors\":\"H.S.C. Wang\",\"doi\":\"10.1109/AERO.1990.109093\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"To provide generic design guidelines for volute antenna elements over a wide range of parameters, a theoretical formulation and algorithm for computing the antenna radiation field have been developed. From these computed field values, the antenna directivity, 3-dB beamwidth, axial ratio, and front/back ratio can be evaluated for the purpose of design tradeoff considerations. The technical approach used is to compute the radiation fields for the helical wires and the straight-end connecting wires, based on a sinusoidal current distribution model along each of the four filaments or wires of the volute. Using axial length as a running variable, a complete tradeoff for the case of the half-turn, half-wavelength volute to meet certain special requirements was considered as an example for design analysis.<<ETX>>\",\"PeriodicalId\":141316,\"journal\":{\"name\":\"IEEE Conference on Aerospace Applications\",\"volume\":\"31 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1990-02-04\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Conference on Aerospace Applications\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO.1990.109093\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Conference on Aerospace Applications","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO.1990.109093","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Theoretical design and predictions of volute antenna performance
To provide generic design guidelines for volute antenna elements over a wide range of parameters, a theoretical formulation and algorithm for computing the antenna radiation field have been developed. From these computed field values, the antenna directivity, 3-dB beamwidth, axial ratio, and front/back ratio can be evaluated for the purpose of design tradeoff considerations. The technical approach used is to compute the radiation fields for the helical wires and the straight-end connecting wires, based on a sinusoidal current distribution model along each of the four filaments or wires of the volute. Using axial length as a running variable, a complete tradeoff for the case of the half-turn, half-wavelength volute to meet certain special requirements was considered as an example for design analysis.<>