Antenna control systems:: From PI to H∞

被引:45
作者
Gawronski, W [1 ]
机构
[1] CALTECH, Jet Prop Lab, Commun Ground Syst Sect, Pasadena, CA 91109 USA
关键词
control systems; control engineering; antennas; pointing systems; reflector antennas; reflector antenna; mechanical factors; linear-quadratic-Gaussian control; H-infinity control;
D O I
10.1109/74.920018
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
This paper discusses the compensation of antenna-pointing errors following the recent analysis and retrofit of the NASA Deep Space Network antenna-control systems. The desired high-frequency communications with spacecraft (at Ka-band) require improved pointing precision over lower-frequency communications (at X-band). The quality of the antenna drives (hardware), the control algorithm (software), and the physical structure of the antenna (in terms of thermal deformations, gravity distortions, encoder mounting, and wind gusts) all influence pointing precision, and create the challenging task of remaining within the required pointing-error budget. Three control algorithms - PI (proportional-and-integral), LQG (linear-quadratic-Gaussian), and H-infinity - are discussed, and their basic properties, tracking precision, and limitations as applied to antenna tracking are addressed. The paper shows that the PI algorithm is simple and reliable, but its performance is limited. It also explains how significant improvements in tracking precision are achieved when implementing the LQG control algorithm or the H-infinity control algorithm. Still, pointing precision attributable to software modification is limited. It is pointed out that an additional increase of tracking precision requires concurrent improvements in the antenna drives.
引用
收藏
页码:52 / 60
页数:9
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