Automatic phase alignment system for a tracking antenna

• US 4,348,676 A
• Filed: 09/09/1980
• Issued: 09/07/1982
• Est. Priority Date: 09/09/1980
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Ford Aerospace & Communications Corporation
• Inventors: Tom, Nelson N.
• Primary Examiner(s): Buczinski, S. C.
• Application Number:
  US06/185,479
• Time in Patent Office: 728 Days
• Field of Search: 343/116, 343/117 R, 343/17.7, 343/16 M, 343/114, 343/114.5
• US Class Current: 342/420
• CPC Class Codes: G01S 3/023 Monitoring or calibrating
• CPC Class Codes: G01S 3/325 Automatic tracking systems
• CPC Class Codes: G01S 3/46 using antennas spaced apart and measuring phase or time difference between signals therefrom, i.e. path-difference systems

Abstract

The tracking signals of a monopulse satellite tracking system are optimized by aligning the phases of the azimuth and elevation channels (the "difference" channels) with the reference (or "sum") channel using an autophase controller and a simulated far field source in the near field. The autophase controller monitors the output of the tracking receiver and adjusts phase shifters along the transmission paths of the azimuth and elevation channels, in a manner to maximize the outputs of the receiver. The simulated far field source provides an alignment signal for the autophase controller. The simulated far field source consists of a signal generator, a near field probe, and near field phase compensators. The probe is positioned to avoid any nulls in the simulated tracking signal for the frequencies of interest. The probe is also positioned to limit the range of the phase shifts introduced by near field placement, for the frequencies of interest. Near field phase shift compensators are used to offset the phase shifts introduced by the use of a near field source instead of a far field source.

Claims

1. An apparatus for phase aligning a steerable directional antenna'"'"'s tracking system having a reference channel and a first tracking error channel, comprising:

a probe connected to a radiation signal generator, said probe placed within the near field aperture of the antenna but off of the antenna'"'"'s boresight axis; and

a phase shifter switchably placed within one of said channels wherein adjustment of said shifter compensates for phase shifts introduced by the placement of the probe.

2. An apparatus as recited in claim 1 wherein the probe is positioned within a plane prescribed by movement along a first axis.

3. An apparatus as recited in claim 1 wherein the probe is positioned within a plane prescribed by movement along an axis from a group consisting of spatially orthogonal axes.

4. The apparatus of claim 1 wherein the antenna comprises a plurality of receiving elements;

wherein the probe is positioned within a region where the differences in the path lengths between the probe and any two elements is greater than zero and less than half the minimum wavelength of radiation tracked by said antenna.

5. The apparatus of claim 1 wherein the antenna comprises a plurality of receiving elements;

wherein the probe is placed so as to limit the variation in the near-field-probe-induced tracking-error-channel phase shifts as a function of frequency within the frequency band of interest.

6. The apparatus of claim 1 further comprising a second tracking error channel and a second phase shifter placed within one of said second tracking error and reference channels for compensating for phase shifts introduced by placement of the probe;

wherein one tracking channel represents the antenna'"'"'s pointing error with respect to a first axis and the other tracking channel represents the antenna'"'"'s pointing error with respect to a second axis spatially orthogonal to the first axis.

7. The apparatus of claim 1 wherein the tracking error channel contains a multiplexed composite of the antenna'"'"'s error signals proportional to pointing errors with respect to each of two orthogonal axes.

8. An automatic phase alignment system for a steerable tracking antenna comprising:

an error channel for communicating a signal proportional to the augular difference between the antenna'"'"'s boresight axis and the direction of an incoming signal;

a first phase shifter having a first input connected to an output of the error channel;

a detector having a first input connected to an output of the phase shifter;

a reference calibration source connected to a second input of the detector;

a controller having an input connected to an output of the detector and an output connected to a control input of the phase shifter, wherein the controller monitors the output of the detector and automatically adjusts the phase shifter to maximize the signal from the detector.

9. The apparatus of claim 8 further comprising:

a probe located within the antenna'"'"'s near field but off the antenna'"'"'s boresight axis and connected to a radiation source; and

a second phase shifter switchably inserted within one of said error channel and calibration source for compensating for phase deviations introduced by the placement of the probe.

10. An automatic phase alignment system for the tracking network of a steerable antenna having a first error channel, a second error channel, and a reference channel, wherein said first and second error channels represent tracking errors with respect to each of two orthogonal axes, comprising:

a first calibration source which inserts a first calibration signal onto the first error channel;

a second calibration source which inserts a second calibration signal onto the second error channel;

a first alignment phase shifter having a control input and a signal input, wherein the signal input is connected to an output of the first error channel;

a second alignment phase shifter having a control input and a signal input, wherein the signal input is connected to an output of the second error channel;

a first error channel detector having a first input connected to an output of the first alignment phase shifter, and a second input connected to an output of the reference channel;

a second error channel detector having a first input connected to an output of the second alignment phase shifter, and a second input connected to said reference channel output; and

an autophase controller having a first input connected to an output of the first error channel detector, a second input connected to an output of the second error channel detector, a first output connected to the control input of the first alignment phase shifter, and a second output connected to the control input of the second alignment phase shifter;

wherein the autophase controller adjusts the first and second alignment phase shifters to respectively maximize the outputs of the first and second error channel detectors.

11. An automatic phase alignment system for a steerable directional antenna having an azimuth error channel, an elevation error channel, and a reference channel, comprising:

an electromagnetic radiation signal generator;

at least one probe connected to the signal generator, said probe placed in the antenna'"'"'s near field within the aperture of the antenna but off the antenna'"'"'s boresight axis;

an azimuth near-field phase shifter switchably inserted within the azimuth error channel to compensate for azimuthal phase shifts introduced by probe placement;

an elevation near-field phase shifter switchably inserted within the elevation error channel to compensate for elevational phase shifts introduced by probe placement;

an azimuth alignment phase shifter having a control input and a signal input, wherein the signal input is connected to an output of the azimuth error channel;

an elevation alignment phase shifter having a control input and a signal input, wherein the signal input is connected to an output of the elevation error channel;

an azimuth error channel detector having a first input connected to an output of the azimuth alignment phase shifter, and a second input connected to an output of the reference channel;

an elevation error channel detector having a first input connected to an output of the elevation alignment phase shifter, and a second input connected to said reference channel output; and

an autophase controller having a first input connected to an output of the azimuth error channel detector, a second input connected to an output of the elevation error channel detector, a first output connected to the control input of the azimuth alignment phase shifter, and a second output connected to the control input of the elevation alignment phase shifter;

wherein the autophase controller adjusts the azimuth and elevation alignment phase shifters to respectively maximize the outputs of the azimuth and elevation error channel detectors.

12. An automatic phase alignment system for a tracking antenna having a reference channel and a multiplexed error channel for conveying signals representative of antenna pointing errors with respect to two orthogonal axes, comprising:

an electromagnetic radiation signal generator;

a probe, connected to the signal generator, placed in the near field aperture of the antenna, but off of the antenna'"'"'s boresight axis;

a near-field compensation phase shifter switchably inserted into one of said channels to compensate for phase shifts introduced between the probe and said shifter; and

a demultiplexer having an input connected to an output of said error channel, a first output containing an error signal representative of the antenna'"'"'s pointing error with respect to said first axis, and a second output containing an error signal representative of the antenna'"'"'s pointing error with respect to said second axis.

13. The system of claim 12 further comprising:

a first-axis error signal detector having a first input connected to said first-axis error signal via a first-axis phase shifter and a second input connected to an output of said reference channel;

a second-axis error signal detector having a first input connected to said second-axis error signal via a second-axis phase shifter and a second input connected to said reference channel output; and

an autophase controller having an input connected to an output of one of said error signal detectors, and further having an output connected to one of said phase shifters.

14. A method for automatically phase aligning the tracking system of a steerable antenna having a reference channel, at least one tracking error channel, and one coherent detector per error channel connected to outputs of each of said reference and tracking channels, comprising the steps of:

inserting a near-field phase compensator into at least one channel;

supplying a calibration signal to a probe positioned within the near field aperture of the antenna but off the antenna'"'"'s boresight axis so as to induce calibration signals in the reference and tracking channels; and

activating an autophase controller connected to a phase shifter associated with each detector, each shifter being connected to a tracking error channel, said controller automatically adjusting each phase shifter so as to maximize the detected amplitude of the tracking error signal associated with said shifter.

15. A method for calibrating the tracking circuitry of a steerable directional tracking antenna, comprising the steps of:

inserting a radiation source within the near-field aperture of said directional antenna but off the antenna'"'"'s boresight axis, said radiation source transmitting radiation within the frequency range of said directional antenna;

receiving said transmitted radiation by at least two receiving elements disposed to accept the signal to be tracked by said antenna;

generating an error signal from said received radiation, said error signal being proportional to the angular difference between the antenna'"'"'s boresight axis and the path connecting said transmitting antenna and one of said receiving elements;

detecting said error signal; and

phase shifting said error signal to maximize the amplitude of the detected error signal.

16. The method of claim 15 wherein said phase shifting is performed by a phase shifter, and further comprising the step of:

initializing said phase shifter by activating transmitting means in the tracking antenna'"'"'s far field and along the tracking antenna'"'"'s boresight axis in lieu of activating said radiation source, and adjusting said phase shifter so as to maximize the detected error signal.