Satellite tracking antenna system
First Claim
1. Apparatus for controlling in response to a control voltage the speed and direction of rotation of a two phase D.C. stepper motor having first and second field windings, said apparatus comprisingmeans for generating first and second sinusoidal drive voltages which are in quadrature phase relationship, said first voltage being applied to said first winding and said second voltage being applied to said second winding, andmeans responsive to said control voltage for varying the frequency of both said first and second drive voltages and reversing the polarity of said first drive voltage, respectively, for varying the speed and direction of rotation of said motor.
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Accused Products
Abstract
A satellite tracking antenna system for use on board ship as part of a maritime communications satellite terminal is disclosed. The system has a directional antenna which is continually trained in the direction of the satellite so as to receive signals therefrom and transmit thereto in spite of the continual rolling, pitching and turning movement of the ship as it travels along its course, even in heavy seas. The system includes a platform which is adapted to be mounted at the head of the mast of the ship. A servo control unit receives position and angular rate signals from roll and pitch sensors mounted on the platform, and serves to counteract pitch and roll without the need for gyroscopic stabilization means so that the platform always remains level regardless of the pitching and rolling of the ship. A structure including the antenna, is mounted on the platform for rotation in azimuth and elevation. A heading input unit receives synchro information from the ship'"'"'s gyrocompass by way of a gyrocompass converter which translates this information into digital form. The heading input unit also receives azimuth information regarding the position of the satellite as well as elevation data, also regarding the position of the satellite. Azimuth and elevation control servos operated by control signals from the heading input unit train the antenna in azimuth and elevation so that it points in the direction of the satellite. Yawing or turning is counteracted by the heading input unit which modifies the azimuth control signal in accordance with the data as to the ship'"'"'s heading from the gyrocompass converter. The direction of the pointing of the antenna, to accommodate slow changes in latitude and longitude as the ship moves along its course which causes a change in satellite position relative to the ship, is accommodated by either changing the elevation and azimuth data provided to the heading input unit or by means of an automatic satellite position update unit which changes the heading input data to the azimuth and elevation servos in accordance with changes in the strength of the signal received by the antenna from the satellite. A system for converting angle data from synchro or step repeaters into digital data which may be used in the gyrocompass converter is also described. A system for controlling the speed and direction of a stepper motor in response to control voltages which does not require tachometers or other feedback control is described in connection with the servo control system in the pitch and roll servo units and in the azimuth and elevation servo units.
30 Citations
10 Claims
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1. Apparatus for controlling in response to a control voltage the speed and direction of rotation of a two phase D.C. stepper motor having first and second field windings, said apparatus comprising
means for generating first and second sinusoidal drive voltages which are in quadrature phase relationship, said first voltage being applied to said first winding and said second voltage being applied to said second winding, and means responsive to said control voltage for varying the frequency of both said first and second drive voltages and reversing the polarity of said first drive voltage, respectively, for varying the speed and direction of rotation of said motor.
Specification