Gu Chunwang, Liu Hao, Yi Min
Key Laboratory of Microwave Remote Sensing, National Space Science Center, Chinese Academy of Sciences, Beijing 100190, China.
University of Chinese Academy of Sciences, Beijing 100049, China.
Micromachines (Basel). 2023 Jan 15;14(1):228. doi: 10.3390/mi14010228.
The microwave interferometric radiometer (MIR) uses aperture synthesis technology to equate multiple small-aperture antennas into a large-aperture antenna to improve spatial resolution. At present, MIR antennas that operate at frequencies above the C-band mostly use horn antennas, waveguide slot antennas, etc., which have the disadvantages of a high profile and large mass. In this paper, a new type of miniaturized, low-profile, and lightweight K-band fan-beam microstrip grid antenna is designed for the airborne campaign of the K-band one-dimensional MIR of a Microwave Imager Combined Active and Passive (MICAP) onboard a Chinese Ocean Salinity Mission (COSM). With a limited size constraint (12.33 mm) on the antenna width, a fan-beam shape antenna pattern was achieved with a 5.34° 3-dB beamwidth in the narrow beam direction and up to a 55° 3-dB beamwidth in the fan-beam direction. A periodic structural unit is proposed in this paper to reduce the design complexity of Taylor weighting, achieving desirable performances on gain (19.1 dB) and sidelobe level (<−20 dB) in the H-plane. Four antenna elements were fabricated and arranged in a non-redundant sparse array. The performance of the four-element sparse array was evaluated with a simulation and real measurement in an anechoic chamber. The coupling between antenna elements was less than −25 dB, and the consistency of phase patterns was better than 3.4°. These results verify the feasibility of the proposed K-band microstrip grid antenna for airborne MIR applications.
微波干涉辐射计(MIR)采用孔径合成技术,将多个小孔径天线等效为一个大孔径天线,以提高空间分辨率。目前,工作在C波段以上频率的MIR天线大多采用喇叭天线、波导缝隙天线等,这些天线存在剖面高、质量大的缺点。本文针对中国海洋盐度探测任务(COSM)机载微波成像仪有源无源组合(MICAP)的K波段一维MIR的机载应用,设计了一种新型的小型化、低剖面、轻量化的K波段扇形波束微带栅天线。在天线宽度有限尺寸约束(12.33毫米)的情况下,实现了扇形波束形状的天线方向图,在窄波束方向上3分贝波束宽度为5.34°,在扇形波束方向上高达55°。本文提出了一种周期性结构单元,以降低泰勒加权的设计复杂度,在H面的增益(19.1分贝)和旁瓣电平(<−20分贝)上实现了理想的性能。制作了四个天线单元并排列成非冗余稀疏阵列。在消声室中通过仿真和实际测量对四元稀疏阵列的性能进行了评估。天线单元之间的耦合小于−25分贝,相位方向图的一致性优于3.4°。这些结果验证了所提出的K波段微带栅天线用于机载MIR应用的可行性。