北京航空航天大学学报
北京航空航天大學學報
북경항공항천대학학보
2001年
1期
12-15
,共4页
单脉冲天线%天线方向图%口面效率%环焦天线%和差通道%双反射面天线
單脈遲天線%天線方嚮圖%口麵效率%環焦天線%和差通道%雙反射麵天線
단맥충천선%천선방향도%구면효솔%배초천선%화차통도%쌍반사면천선
分析了单脉冲环焦天线差通道性能较差的原因,推荐了适用的和差口径分布函数,得出了所需馈源差方向图计算式, 提出了和差性能一体化设计步骤.为了验证理论方法的正确性,以3.5?m变极化赋形单脉冲环焦天线为例,用本文提出的方法修改设计,使“和差矛盾”由6.5?dB减为4.2?dB,差方向图分离角由1.9°降为1.4°.因此, 使用特殊设计的单脉冲馈源可望将归一化差斜率提高到1.4.
分析瞭單脈遲環焦天線差通道性能較差的原因,推薦瞭適用的和差口徑分佈函數,得齣瞭所需饋源差方嚮圖計算式, 提齣瞭和差性能一體化設計步驟.為瞭驗證理論方法的正確性,以3.5?m變極化賦形單脈遲環焦天線為例,用本文提齣的方法脩改設計,使“和差矛盾”由6.5?dB減為4.2?dB,差方嚮圖分離角由1.9°降為1.4°.因此, 使用特殊設計的單脈遲饋源可望將歸一化差斜率提高到1.4.
분석료단맥충배초천선차통도성능교차적원인,추천료괄용적화차구경분포함수,득출료소수궤원차방향도계산식, 제출료화차성능일체화설계보취.위료험증이론방법적정학성,이3.5?m변겁화부형단맥충배초천선위례,용본문제출적방법수개설계,사“화차모순”유6.5?dB감위4.2?dB,차방향도분리각유1.9°강위1.4°.인차, 사용특수설계적단맥충궤원가망장귀일화차사솔제고도1.4.
The relatively poor performance of difference channel of a monopulse ring-focus antenna is accounted for, suitable aperture distribution functions are recommended, formulae of feed difference pattern needed are presented and sum-difference unified design method is put forward. To testify the theoretical method, the authors take a 3.5m C-band monopulse shaped ring-focus antenna with dual-polarization as an example. By using the presented method, the gain difference between the sum channel and the different channel is reduced from 6.5dB to 4.2dB , and the separation angle of the apexes of the different pattern of the antenna from 1.9° to 1.4°. Therefore, the normalized slope of difference pattern arrives at 1.4 with a particular monopulse feed.