IP Library Granted Patent US 9,391,356
Granted Patent B2
US 9,391,356 · App. 13/912,186 · Granted Jul 12, 2016

Feature in antenna pattern for pointing and orientation determination

Inventor: David Rochblatt (Long Beach, CA)
Assignee: California Institute of Technology
H01Q1/1257
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Quick Facts
Patent No.
US 9,391,356
App. No.
13/912,186
Granted
Jul 12, 2016
Kind
B2
Abstract

Systems and methods for antenna pointing are disclosed. A transmit antenna system having an adjustable boresight transmits a signal exhibiting a far-field pattern including a feature (e.g. a V-Notch) in a polarization of the signal disposed at a fixed position off a beam peak of the far-field pattern of the signal. A receive antenna system scans across the far-field pattern of the signal in the polarization to locate the feature and determine a pointing error of the adjustable boresight therefrom. The system may be applied to a cross-polarization of the signal where a co-polarization of the signal is simultaneously used for telecommunication.

Claims (27)

1. An apparatus for determining antenna pointing, comprising:

a transmit antenna system for transmitting a signal having an adjustable boresight and exhibiting a far-field pattern including a feature in a polarization component of the far-field pattern disposed at a fixed position off a beam peak of the far-field pattern; and

a receive antenna system for scanning across the far-field pattern in the polarization component to locate the feature and determine a pointing error of the adjustable boresight therefrom;

wherein the feature of the far-field pattern comprises a notch having a depth relative to a main lobe of the far-field pattern varying with an angle of the fixed position off the boresight.

2. The apparatus of claim 1 , wherein the feature disposed at the fixed position off the beam peak of the far-field pattern is mapped with the transmit antenna system installed to include any multipath effects.

3. The apparatus of claim 1 , wherein the pointing error is transmitted to the transmit antenna system and the boresight is adjusted to correct the pointing error.

4. The apparatus of claim 1 , wherein the transmit antenna system is installed on a spacecraft and the receive antenna is disposed at a ground station.

5. The apparatus of claim 1 , wherein the polarization component having the feature in the far-field pattern is a cross-polarization component and a co-polarization component is simultaneously used to communicate while the receive antenna system determines the pointing error.

6. The apparatus of claim 5 , wherein the co-polarization component comprises a right circular polarization (RCP) and the cross-polarization component comprises a left circular polarization (LCP).

7. The apparatus of claim 1 , wherein the feature in the far-field pattern of the polarization component is switchably activated.

8. The apparatus of claim 7 , wherein the polarization component having the feature in the far-field pattern is a co-polarization component and the feature is only temporarily activated for the receive antenna system to determine the pointing error.

9. A method for determining antenna pointing, comprising:

transmitting a signal with a transmit antenna system having an adjustable boresight and exhibiting a far-field pattern including a feature in a polarization component of the far-field pattern disposed at a fixed position off a beam peak of the far-field pattern; and

scanning across the far-field pattern in the polarization component with a receive antenna system to locate the feature and determine a pointing error of the adjustable boresight therefrom;

wherein the feature of the far-field pattern comprises a notch having a depth relative to a main lobe of the far-field pattern varying with an angle of the fixed position off the boresight.

10. The method of claim 9 , further comprising mapping the feature disposed at the fixed position off the beam peak of the far-field pattern with the transmit antenna system installed to include any multipath effects.

11. The method of claim 9 , further comprising transmitting the pointing error to the transmit antenna system and adjusting the boresight to correct the pointing error.

12. The method of claim 9 , wherein the transmit antenna system is installed on a spacecraft and the receive antenna is disposed at a ground station.

13. The method of claim 9 , wherein the polarization component having the feature in the far-field pattern is a cross-polarization component and a co-polarization component is simultaneously used to communicate while the receive antenna system determines the pointing error.

14. The method of claim 13 , wherein the co-polarization component comprises a right circular polarization (RCP) and the cross-polarization component comprises a left circular polarization (LCP).

15. The method of claim 9 , wherein the feature in the far-field pattern of the polarization component is switchably activated.

16. The method of claim 15 , wherein the polarization component having the feature in the far-field pattern is a co-polarization component and the feature is only temporarily activated for the receive antenna system to determine the pointing error.

17. An apparatus for determining antenna pointing, comprising:

a transmit antenna system means for transmitting a signal having an adjustable boresight and exhibiting a far-field pattern including a feature in a polarization component disposed at a fixed position off a beam peak of the far-field pattern; and

a receive antenna system means for determining a pointing error of the adjustable boresight from scanning across the far-field pattern in the polarization component to locate the feature;

wherein the feature of the far-field pattern comprises a notch having a depth relative to a main lobe of the far-field pattern varying with an angle of the fixed position off the boresight.

18. The apparatus of claim 17 , wherein the feature of the far-field pattern is mapped with the transmit antenna system means installed to include any multipath effects.

Assignments (2)
CONFIRMATORY LICENSE Recorded Aug 12, 2013
From: CALIFORNIA INSTITUTE OF TECHNOLOGY
To: NASA
Reel/Frame 031138/0926 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 6, 2013
From: ROCHBLATT, DAVID
To: CALIFORNIA INSTITUTE OF TECHNOLOGY
Reel/Frame 030563/0604 →
Continuity (2)
Provisional Application 61656433 · Jun 6, 2012
Related Publication 20130328721A1 · Dec 12, 2013