This paper discusses the compensation of antenna-pointing errors following
the recent analysis and retrofit of the NASA Deep Space Network antenna-con
trol systems. The desired high-frequency communications with spacecraft (at
Ka-band) require improved pointing precision over lower-frequency communic
ations (at X-band). The quality of the antenna drives (hardware), the contr
ol algorithm (software), and the physical structure of the antenna (in term
s 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-quad
ratic-Gaussian), and H-infinity - are discussed, and their basic properties
, tracking precision, and limitations as applied to antenna tracking are ad
dressed. The paper shows that the PI algorithm is simple and reliable, but
its performance is limited. It also explains how significant improvements i
n tracking precision are achieved when implementing the LQG control algorit
hm or the H-infinity control algorithm. Still, pointing precision attributa
ble to software modification is limited. It is pointed out that an addition
al increase of tracking precision requires concurrent improvements in the a
ntenna drives.