Satellite tracking antenna apparatus

• US 4,156,241 A
• Filed: 04/01/1977
• Issued: 05/22/1979
• Est. Priority Date: 04/01/1977
• Status: Expired due to Term

• Current Assignee: Scientific-Atlanta Incorporated (Cisco Systems, Inc.)
• Original Assignee: Scientific-Atlanta Incorporated (Cisco Systems, Inc.)
• Inventors: Wilson, Robert J., Mobley, Joseph G.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US05/783,582
• Time in Patent Office: 781 Days
• Field of Search: 343/100 ST, 343/100 AD, 343/117 R, 343/709, 343/765, 318/649
• US Class Current: 342/352
• CPC Class Codes: G01S 3/44 the adjustment being varied periodically or continuously until it is halted automatically when the desired condition is attained
• CPC Class Codes: H01Q 1/18 Means for stabilising antennas on an unstable platform
• CPC Class Codes: H01Q 1/34 Adaptation for use in or on ships, submarines, buoys or torpedoes for subaqueous use H01Q1/04
• CPC Class Codes: H01Q 3/08 for varying two co-ordinates of the orientation

Abstract

Satellite tracking apparatus for use on board ship as part of a maritime communications satellite terminal is disclosed. A directional antenna which is adapted to be trained in the direction of the satellite so as to be in communication therewith is mounted so as to be positioned about three axes, namely train, elevation, and cross-level axes. The mount also has a fourth axis which is parallel to or collinear with one of the other axes. This fourth axis may be a level axis which is movable with the antenna. A stable platform is movable with and rotatable about the level axis. Sensors on this platform provide outputs to servo controllers which rotate the antenna about the elevation and cross-level axes to maintain the platform stable. An azimuth sensor such as a gyro compass and sensors responsive to angular motion with respect to the train axis may also be mounted on the platform and provide outputs to a servo controller which controls the bearing or azimuth position of the antenna. An open loop control is provided for the level axis which establishes an equivalent angle between the stable platform and the true elevation line of sight (an angle equal to but opposite from the true elevation angle to the satellite). A mislevel is thereby created and sensed by the sensor for the elevation axis which provides an output that activates the elevation axis servo controller to reduce the mislevel to zero and null, thereby achieving the desired elevation of the antenna. The antenna is stabilized and decoupled from the motions (roll, pitch and yaw) of the ship and changes in the ship'"'"'s heading, in that the sensors are mounted on the stable platform which moves with the antenna. The need for coordinate conversion computers responsive to sensors strapped down to the deck or other ship structure and for alignment of the antenna axes with the pitch or roll axis of the ship is also eliminated. The rotation of the antenna about its boresight axis is eliminated; thus avoiding misalignment between the polarization of the antenna and the satellite signals.

Claims

1. Apparatus for controlling the position of a body which comprises

means for mounting said body for rotation about at least two mutually orthogonal axes,

means rotatable with said body about said axes defining a platform rotatable with respect to said body about a third axis parallel to or collinear with a first of said two axes,

sensor means mounted on said platform for sensing orientation of said body about each of said two axes with respect to the vertical,

servo control means responsive to said sensor means for rotating said body about said two axes to maintain said platform level,

means for rotating said platform about said third axis to vary the relative angle between said third axis and said first axis, whereby said sensor means operate said servo control means to rotate said body to change the attitude thereof to correspond to said relative angle,

means also mounted upon said platform for sensing the angular position of said body about a fourth axis, which is mutually perpendicular to said two axes, relative to a reference position and providing an output corresponding thereto,

said servo control means including means responsive to said output for rotating said body about said fourth axis to said reference position, and

means for varying said output to maintain said body at other positions relative to said reference position.

2. Apparatus for controlling the position of a body which comprises

means for mounting said body for rotation about at least two mutually orthogonal axes,

means rotatable with said body about said axes defining a platform rotatable with respect to said body about a third axis parallel to or collinear with a first of said two axes,

sensor means mounted on said platform for sensing orientation of said body about each of said two axes with respect to the vertical,

servo control means responsive to said sensor means for rotating said body about said two axes to maintain said platform level,

means for rotating said platform about said third axis to vary the relative angle between said third axis and said first axis, whereby said sensor means operate said servo control means to rotate said body to change the attitude thereof to correspond to said relative angle,

said sensor means including means mounted on said platform responsive to the angular motion of said body with respect to said two axes,

means also mounted upon said platform for sensing the angular position of said body about a fourth axis, which is mutually perpendicular to said two axes, with respect to a reference position and providing an output corresponding thereto,

means mounted upon said platform for sensing the angular motion of said body about said fourth axis and for providing an output corresponding thereto, said servo control means including means responsive to said outputs from said means for sensing said angular position and motion about said fourth axis to rotate said body to maintain said body at said reference position, and

means for varying said output from said angular position sensing means to which said servo control means is responsive to rotate said body about said fourth axis to positions other than said reference position.

3. The invention as set forth in claim 2 wherein said angular position sensing means is a gyro compass.

4. For use on a ship or the like for mounting a directional antenna which is adapted to be trained to point to a satelliteborne transmitting station to maintain communication therewith, said apparatus comprising means mounting said antenna for rotation about a plurality of mutually orthogonal axes, means coupled to said mounting means for rotating said antenna about each of said axes, means for sensing the orientation of said antenna, means defining a platform for mounting said sensing means for movement with said antenna and for rotation about an axis parallel to or collinear with one axis of said plurality of axes, servo control means responsive to said sensing means for operating said rotating means to keep said platform means level, means for rotating said platform means to change the attitude thereof about the axis of rotation of said platform whereby to cause said servo control means to change the attitude of said antenna with respect to said one axis, said antenna being directional along a boresight axis, said plurality of axes includes an elevation axis which is perpendicular to the boresight axis of said antenna and a cross level axis, the axis of said platform being the level axis, said means for rotating said platform means being operative to cause said servo control means to vary the elevation angle of said boresight axis, said mounting means mounting said antenna for rotation about a train axis so that said boresight axis is movable in azimuth, said rotating means including azimuth motor means coupled to said mounting means for rotating said antenna about said train axis, compass means mounted on said platform means for providing an azimuth output corresponding to the relative bearing of said platform means with respect to a reference direction, said servo control means including a train channel for applying said azimuth output to said azimuth motor means for rotating said antenna about said train axis, and means for setting the direction of said antenna in azimuth included in said train channel for varying said azimuth output to correspond to an azimuth setting.

5. The invention as set forth in claim 4 wherein said sensing means includes a rate sensor mounted on said platform means and responsive to the angular motion of said platform about said train axis, said train channel having a position loop responsive to the output from said varying means and a rate loop responsive to the output from said rate sensor, said loops providing said azimuth output for controlling said azimuth motor means.

6. For use on a ship or the like for mounting a directional antenna which is adapted to be trained to point to a satelliteborne transmitting station to maintain communication therewith, said apparatus comprising means mounting said antenna for rotation about a plurality of mutually orthogonal axes, means coupled to said mounting means for rotating said antenna about each of said axes, means for sensing the orientation of said antenna, means defining a platform for mounting said sensing means for movement with said antenna and for rotation about an axis parallel to or collinear with one axis of said plurality of axes, servo control means responsive to said sensing means for operating said rotating means to keep said platform means level, means for rotating said platform means to change the attitude thereof about the axis of rotation of said platform whereby to cause said servo control means to change the attitude of said antenna with respect to said one axis, said antenna being directional along a boresight axis, said plurality of axes includes an elevation axis which is perpendicular to the boresight axis of said antenna and a cross level axis, the axis of said platform being the level axis, said means for rotating said platform means being operative to cause said servo control means to vary the elevation angle of said boresight axis, said level sensor means including a first level sensor responsive to the position of said platform with respect to said elevation axis for providing an elevation position output and a second level sensor responsive to the position of said platform with respect to said cross-level axis for providing a cross level position output, said rotating means including elevation motor means coupled to said mounting means for rotating said antenna about said elevation axis, cross-level motor means coupled to said mounting means for rotating said antenna about said cross-level axis, said servo control means including an elevation channel and a cross-level channel respectively for applying said first level sensor output to said elevation motor means and said second level sensor output to said cross level motor means, said sensor means also including a first rate sensor responsive to angular motion of said platform means about said elevation axis and a second rate sensor responsive to angular motion of said platform means about said cross level axis, said elevation channel including a position loop responsive to said first level sensor and a rate loop responsive to said first rate sensor, said loops in said elevation channel providing a signal for controlling said elevation motor means, said cross-level channel including a position loop responsive to said second level sensor and a rate loop responsive to said second rate sensor, and said loops in said cross level channel providing a signal for controlling said cross level motor means.

7. The invention as set forth in claim 6 wherein said means for rotating said platform means includes a level motor means mounted to drive said platform means about said level axis, means for setting the elevation angle of said antenna bore sight axis providing a control signal for operating said motor to rotate said platform means in a sense opposite to the sense in which said elevation angle is to be varied to reach said elevation setting.

8. The invention as set forth in claim 7 including means responsive to signals received from said satellite by said antenna for successively providing step track signals representing the strength of said received signal, and means included in said elevation angle setting means responsive to said step track signals for changing said control signals in the sense to change said elevation angle whereby to increase the strength of said received signals.

9. The invention as set forth in claim 8 and wherein said mounting means also mounts said antenna for rotation about a train axis so that said boresight axis is movable in azimuth, said rotating means including motor means coupled to said mounting means for rotating said antenna about said train axis, compass means mounted on said platform means for providing an azimuth output corresponding to the relative bearing of said platform means with respect to a reference direction, said servo control means including a train channel for applying said azimuth output to said motor means for rotating said antenna about said train axis, and means for setting the direction of said antenna in azimuth included in said train channel for varying said azimuth output to correspond to an azimuth setting, and means included in said azimuth direction setting means responsive to said step track signals for varying said azimuth output to change the position of said antenna in azimuth whereby to increase the strength of said received signals.

10. For use on a ship or the like, apparatus for mounting a directional antenna having a boresight axis which is adapted to be trained towards a satellite-borne transmitting station to maintain communication therewith, said apparatus comprising

a pedestal adapted to be secured to the structure of said ship,

a section journaled on the pedestal for rotation about a train axis perpendicular to the deck of said ship,

a yoke rotatably mounted on said section for rotation about a cross-level axis,

a support structure in which said antenna is held, said support structure being mounted on said yoke for rotation about an elevation axis,

said elevation axis, cross elevation and train axes being mutually orthogonal, said elevation axis also being orthogonal to said boresight axis,

a unit mounted on said support structure for rotation about a level axis which extends in the same direction as said elevation axis and in mutually orthogonal relationship with said cross-level and train axes,

separate train, cross-level elevation and level motors respectively in rotational driving relationship with said section, said yoke and said support structure,

an elevation level sensor, a cross level sensor, and an azimuth sensor mounted in said unit, said unit defining a level platform for said sensors, said sensors providing a separate elevation, cross level and azimuth outputs corresponding to the angular position of said platform with respect to said elevation and cross-level axes and with respect to a reference azimuthal direction,

an elevation channel and a cross level channel respectively responsive to said elevation sensor output and said cross level sensor output for controlling said elevation and cross level motors to rotate said support structure and said yoke to maintain said platform level,

means for setting the elevation angle of said boresight axis operative to control said level motor to rotate said level platform to an angle equal and opposite to said elevation angle whereby to cause said elevation sensor to provide an elevation output to said elevation channel to cause said elevation motor to rotate said support structure until said bore sight axis reaches said elevation angle, and

a train channel responsive to said azimuth sensor output and to a control signal corresponding to the direction azimuth of said boresight axis for controlling said azimuth motor to rotate said section until it reaches said azimuth direction.

11. The invention as set forth in claim 10 wherein said support structure has a framework having a base, said antenna being disposed in said framework upon said base on one side thereof, a plurality of blocks extending from the opposite side of said base, a shaft held in said blocks, said yoke having bearings in which said shaft is journaled, the axis of said shafts being collinear with said elevation axis, said elevation motor being disposed on said yoke and being coupled to said shaft.

12. The invention as set forth in claim 11 wherein said section has upwardly extending arms, said yoke has a shaft attached thereto, bearings disposed on said arms in which said yoke shaft is mounted, said cross level motor being disposed on one of said arms and being coupled to said yoke shaft, said yoke shaft being disposed below said elevation shaft and said yoke shaft being collinear with said cross level axis.

13. The invention as set forth in claim 12 wherein said train motor is mounted on said section with the axis of said motor parallel to said train axis and coupled in driving engagement with said pedestal.

14. The invention as set forth in claim 10 wherein said unit comprises a housing, a shaft on said support structure, said shaft being disposed along said elevation axis, bearings rotatably mounting said housing on said shaft, said level motor being disposed in said housing and having a shaft disposed along an axis parallel to and spaced from said elevation axis shafts, a ring gear secured to said support structure gearing means including a pinion connected to said level motor shaft, said pinion being in engagement with said ring gear whereby to rotate said housing about said level axis.

15. The invention as set forth in claim 14 wherein said azimuth sensor is a gyro compass which is disposed in said housing.

16. The invention as set forth in claim 15 wherein said apparatus further comprises an elevation rate sensor, a cross elevation rate sensor, and a yaw rate sensor, all mounted in said housing, said elevation, cross level and train channels each having a position loop amplifier and a rate loop amplifier, means for applying the level sensor output to said position loop amplifier inputs, means for applying said position loop amplifier output and said rate sensor output to the input of said rate loop amplifier, and means for controlling said motors in accordance with the output of said rate loop amplifier.

17. The invention as set forth in claim 16 wherein said apparatus includes step track controller means responsive to a signal received from said satellite by said antenna for providing step track control signals, and means for applying said step track control signals to the position loop amplifier of said train channel and to said level motor so as to vary said level control signal and said azimuth sensor signal to cause said antenna to rotate in azimuth and elevation in a direction to increase the strength of said received signal.