期刊文献+

构架式可展天线电性能研究

Electro-magnetic Performance Research on Tetrahedron Truss Antenna
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摘要 提出了一种构架单元式的展开桁架天线,对构架式可展天线的电性能进行了研究,以确定较优的设计参数和结构方案,针对可展反射面形态的具体特点,基于几何光学原理,推导了可展天线远场的电场强度公式,将口径面划分成矩形网格,用数值方法对远场场强进行积分,得到天线反射面的方向图.进而编制相应程序,用于分析不同设计参数的构架式天线反射面的电性能.该方法直接将结构变形与天线电性能相联系,避免了通过均方根换算带来的额外误差,使得设计更准确.此方法同样适用于标准抛物面或者任何已知缺陷反射面的辐射场计算. Large deployable truss antennas have extensive applications in communication satellites and space stations. This paper deals with a kind of deployable truss antenna that consists of tetrahedral niodules. Electro-magnetic performance of tetrahedron truss deployable antenna is researched, to optinfize design parameter and structure precept. According to the features of the deployable reflector configuration and the geometry optical theory, the computing arithmetic of the electro-field intensity of the tetrahedron truss antenna is formulized. Then the paraboloid reflector is separated to form rectangular grid on the aperture plane and the integral of the far-field is conducted with the analytical method. Finally far-field pattern of antenna reflector is obtained. The corresponding program is designed and used to analyze far-field pattern of truss antenna with different design parameter. This method directly related the structure with the electro-magnetic field, which improves the design by leaving out the RMS value. So the design process is more accurate. This program can be applied to analyze the reflector radiation field of standard reflector or any reflector which distortion is already described.
出处 《空间科学学报》 CAS CSCD 北大核心 2011年第5期687-692,共6页 Chinese Journal of Space Science
关键词 构架式可展天线 电性能 方向图 参数优化 Tetrahedron truss antenna Electro-magnetic performance, Far-field pattern, Parameter optimize
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参考文献9

  • 1Miura K,Furuya H.Variable geometry truss and space crane arm[J].Acta Astron.,1985,12(7):599-607.
  • 2Miura K,Furuya H.Adaptive structure concept for future space applications[J].AIAA Journal,1988,(268):995-1002.
  • 3Rahmat-samii Y.A Comparison between GO/Aperturefield and physical-optics methods for offset reflectors[J].IEEE Trans.Alitenn.4s Prop.,1984,32(3):301-307.
  • 4Rahmat-samii Y.Nonuniform sampling techniques for antenna applications[J].IEEE Trans.Anten.Prop.,1984,35(3):268-280.
  • 5Guan Fuling.Basic Study on Structural Shape Analysis of Spacial Struss and Applications on Communication Engineering[D].Japan: Tokyo University,Doctoral dissertation,1989.
  • 6Alan R.Cherrette a method for producing a shaped contour tadiation pattern using a single shaped reflector and single feed[J].IEEE Trans.Aanten.Prop.,1989,37(6):698-707.
  • 7Cherrette A R,Chang D C D.Phased array contour beam shaping by phase optimization[C]//Antennas propagate.Vancouver BC: Symp.int.symp.Dig.,1985,475-478.
  • 8杨可忠,杨智友.章日荣.现代面天线新技术[M].北京:人民邮电出版社,1990.
  • 9关富玲,侯国勇,赵孟良.构架式可展开天线结构设计的程序实现[J].工程设计学报,2006,13(2):108-113. 被引量:13

二级参考文献6

  • 1岳建如,关富玲,陈向阳.大型可展构架式星载抛物面天线结构设计[J].浙江大学学报(工学版),2001,35(2):179-179. 被引量:11
  • 2EIDEN M, BRUNNER O Stavrinidis. Deployment analysis of olympus astromast and comparison with test measurements[J]. J Spacecraft & Rocket, 1987,24(1):63-38.
  • 3HERR R W, HORNER G C, Deployment Test of A 36-Element Tetrahedral Truss Module[R]. NASA-CP-2168-V-1. Vought Corp, Dallas Texas, 2nd Annual Technical Review
  • 4TAKAGWKI Kitamure, KAKUMA Okazaki, Development of a "hingless mast" and its application[J]. Acta Astronautica, 1988,17 ( 3 ): 341 - 346.
  • 5LAI C Y, PELLEGRINO S. Feasibility Study of a Deployable Mesh Reflector [R]. Cambridge. Deployable Structure Laboratory Department of Engineering, University of Cambridge, 2001.
  • 6张京街,关富玲,胡其彪.大型切割旋转抛物面展开结构的设计[J].工程设计学报,2000,7(1):46-48. 被引量:10

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