Design and performance of the monopulse control system

被引：6

作者：

Gawronski, W ^{[1
]}

Gudim, MA ^{[1
]}

机构：

[1] CALTECH, Jet Prop Lab, Commun Ground Syst Sect, Pasadena, CA 91109 USA

来源：

IEEE ANTENNAS AND PROPAGATION MAGAZINE | 1999年 / 41卷 / 06期

关键词：

servosystems; space vehicle tracking; monopulse radar; monopulse antenna;

D O I：

10.1109/74.815317

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

Ka-band (32 GHz) monopulse tracking has been chosen for the upcoming NASA missions. This decision requires an increased pointing accuracy for the Deep Space Network antenna servo systems that can be maintained in a noisy environment. The noise sources include wind gusts, encoder imperfections, and receiver noise. This article describes the selection of the position and monopulse controllers for the improved tracking accuracy, and presents the results of linear and non-linear simulations to confirm that servo performance will meet the requirements.

引用

页码：40 / 50

页数：11

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