发明名称 Tracking controller for three-axis mount antenna systems.
摘要 <p>In a satellite tracking control system, a receiver derirves a pair of elevation (EL) and cross-elevation (XEL) tracking error signals having a quadratic relationship in a coordinate system from a signal received from a polar-orbital satellite. Elevation and cross-elevation motors are respectively controlled in response to the elevation (EL) and cross-elevation (XEL) tracking error signals. An azimuth controller derives an azimuth control signal from angle data representing the angles of the antenna about the azimuth, elevation and cross-elevation axes detected by angle detectors. Preferably, the antenna is rotatable about the elevation (EL) axis in the range between zero and l80 degrees.</p>
申请公布号 EP0246635(A2) 申请公布日期 1987.11.25
申请号 EP19870107347 申请日期 1987.05.20
申请人 NEC CORPORATION 发明人 NAKAYAMA, MAKOTO
分类号 G01S3/42;H01Q3/08 主分类号 G01S3/42
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