卫星通信系统多波段镜像天线激振器的构建

D. D. Gabriél'yan, V. I. Demchenko, A. E. Korovkin, D. Y. Razdorkin, Yu.A. Gvozdyakov, Yu. I. Poltavets
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摘要

. 本文的目的是证明在不同重叠频带组合下多波段镜像天线波形喇叭激励器参数的优化方法及其在实践中的实现。研究了卫星通信系统中多波段收发镜像天线的波形角馈源系统的构建问题。通过对卫星通信系统性能指标与无线电信道能量特性的相互关系分析,可以确定接收地面站多波段镜像天线及其激励器的性能指标。多波段镜像天线的性能指标采用考虑各重叠波段天线噪声q因子的乘函数形式,由于接收信号的去极化效应和SC自动跟踪过程中天线指向的不准确,两个辅助因素决定了有效噪声q因子的降低。采用波纹喇叭作为多波段镜像天线的激励器,激励主H 11模式和最高H 21模式,允许人们为具有不同功能的多波段镜像天线创建激励器。重点介绍了基于极值和单脉冲的可编程制导和自动跟踪模式。研究了不同轨道卫星通信系统激振器设计的考虑。
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Building of Exciters of Multiband Mirror Antennas for Satellite Communication Systems
. The objective of the paper is to justify the approach to optimization of the parameters of the corrugated horn based exciters of multiband mirror antennas for different combinations of the overlapping bands and their realization in practice. The issues of building the feed systems based on the corrugated horns for multiband transceiving mirror antennas of satellite communication systems are studied. The conducted interrelation analysis of performance indicators of the satellite communication system with energy characteristics of the radio channel enabled one to justify the performance indicator of the multiband mirror antenna of the receiving ground station and its exciters. The performance indicator of the multiband mirror antenna is in the form of a multiplicative function taking account of the antenna noise Q-factor in each of the overlapping bands, and two co-factors determining the decrease in the effective noise Q-factor due to depolarization effects of the received signals and inaccuracy in antenna pointing during autotracking of SC. Employing a corrugated horn as exciters of multiband mirror antennas exciting the main H 11 mode and the highest H 21 mode permits one to create exciters for multiband mirror antennas with different functional capabilities, in particular with the modes of programmable guidance and autotracking based on the extreme and monopulse methods. The considerations of designing the exciters for communication systems with satellites in various types of orbits are studied.
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