Ground-based satellite antenna pointing system

• US 9,853,356 B2
• Filed: 09/25/2014
• Issued: 12/26/2017
• Est. Priority Date: 09/26/2013
• Status: Active Grant

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Orbital Sciences Corporation (Northrop Grumman Corporation)
• Inventors: Yao, Huiwen, Case, George
• Primary Examiner(s): Sotomayor, John B
• Application Number:
  US14/496,071
• Publication Number:
  US 20160365629A1
• Time in Patent Office: 1,188 Days
• Field of Search: 342354, 342355, 342358, 342359, 342385, 342386
• CPC Class Codes: G01S 19/13 Receivers
• CPC Class Codes: H01Q 1/1257 using the received signal strength
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 3/08 for varying two co-ordinates of the orientation
• CPC Class Codes: H04B 7/18519 Operations control, administration or maintenance
• CPC Class Codes: H04B 7/2041 Spot beam multiple access

Abstract

The present application includes systems and methods for determining pointing error of a satellite antenna. In one aspect a method for determining pointing error of a satellite antenna includes receiving, at a receiving station, a pointing error signal formed by the antenna and transmitted from a satellite, wherein the pointing error signal includes a first beacon (reference) signal and a modulated second beacon (error) signal. The receiving station may demodulate the received pointing error signal to recover the second beacon signal with respect to the first beacon signal, and based at least in part on the demodulated beacon signal, the receiving station may determine the pointing error of the satellite antenna.

Claims

1. A method for determining pointing error of a satellite antenna,

the method comprising:

receiving, at a receiving station, a pointing error signal transmitted from a satellite, wherein the pointing error signal includes a first beacon signal and a modulated second beacon signal both transmitted from the satellite simultaneously at a first frequency and from a single antenna;

demodulating, using a control circuitry, the received pointing error signal to recover the first beacon signal and the modulated second beacon signal; and

determining, using the control circuitry, a pointing error based at least in part on the first beacon signal and the modulated second beacon signal, wherein determining the pointing error based at least in part on the first beacon signal and the modulated second beacon signal comprises;

comparing a magnitude of the modulated second beacon signal with a magnitude of the first beacon signal; and

determining a phase of at least one of the first beacon signal and the modulated second beacon signal.

2. The method of claim 1, further comprising:

determining, using the control circuitry, a control signal based on the pointing error; and

transmitting the control signal to the satellite, wherein the control signal includes commands to modify an orientation of the satellite antenna.

3. The method of claim 1, wherein comparing the magnitude of the modulated second beacon signal with the magnitude of the first beacon signal comprises taking a difference in magnitude of the first beacon signal and the modulated second beacon signal.

4. The method of claim 1, wherein determining the pointing error based at least in part on the first beacon signal and the modulated second beacon signal further comprises:

determining a direction of the pointing error based on the determined phase; and

determining a magnitude of the pointing error based on the comparison of the magnitude of the modulated second beacon signal with the magnitude of the first beacon signal.

5. The method of claim 1, wherein at least one of the first beacon signal and the modulated second beacon signal is configured to have substantially zero magnitude along a boresight axis of the satellite antenna and a substantially non-zero magnitude off of the boresight axis of the satellite antenna.

6. The method of claim 1, wherein the modulated second beacon signal is modulated using one of, phase modulation, frequency modulation, or amplitude modulation.

7. The method of claim 1, wherein the modulated second beacon signal is modulated using a first phase angle and a second phase angle, and wherein the first phase angle is 0 degrees, and wherein the second phase angle is 180 degrees.

8. The method of claim 1, wherein the pointing error signal is generated by combining the first beacon signal and the modulated second beacon signal in a spatial domain.

9. A system for determining pointing error of a satellite antenna, the system comprising:

a receiver in communication with a satellite configured to receive a pointing error signal transmitted from the satellite, wherein the pointing error signal includes a first beacon signal and a modulated second beacon signal both transmitted from the satellite simultaneously at a first frequency and from a single antenna;

control circuitry configured to;

demodulate the received pointing error signal to recover the first beacon signal and the modulated second beacon signal; and

determine a pointing error based at least in part on the first beacon signal and the modulated second beacon signal, wherein the control circuitry being configured to determine the pointing error based at least in part on the first beacon signal and the modulated second beacon signal includes being configured to;

compare a magnitude of the modulated second beacon signal with a magnitude of the first beacon signal; and

determine a phase of at least one of the first beacon signal and the modulated second beacon signal.

10. The system of claim 9, wherein the control circuitry is further configured to:

determine a control signal based on the pointing error; and

transmit the control signal to the satellite, wherein the control signal includes commands to modify an orientation of the satellite antenna.

11. The system of claim 9, wherein the control circuitry is configured to compare the magnitude of the modulated second beacon signal with the magnitude of the first beacon signal by taking a difference in magnitude of the first beacon signal and the modulated second beacon signal.

12. The system of claim 9, wherein the control circuitry is further configured to determine the pointing error based at least in part on the first beacon signal and the modulated second beacon signal by:

determining a direction of the pointing error based on the determined phase; and

determining a magnitude of the pointing error based on the comparison of the magnitude of the modulated second beacon signal with the magnitude of the first beacon signal.

13. The system of claim 9, wherein at least one of the first beacon signal and the modulated second beacon signal is configured to have substantially zero magnitude along a boresight axis of the satellite antenna and a substantially non-zero magnitude off of the boresight axis of the satellite antenna.

14. The system of claim 9, wherein the modulated second beacon signal is modulated using one of, phase modulation, frequency modulation, or amplitude modulation.

15. The system of claim 9, wherein the modulated second beacon signal is modulated using a first phase angle and a second phase angle wherein the first phase angle is 0 degrees, and wherein the second phase angle is 180 degrees.

16. The system of claim 9, wherein the pointing error signal is generated by combining the first beacon signal and the modulated second beacon signal in a spatial domain.

17. A system for determining pointing error of a satellite antenna, the system comprising:

a satellite including control circuitry and an antenna, the control circuitry including;

a tracking beacon configured to generate an initial beacon signal at a first frequency;

a processor communicatively coupled to the tracking beacon to receive the generated tracking signal, the processor including a splitter configured to split the initial beacon signal into a first beacon signal and a second beacon signal; and

a phase modulator communicatively coupled to the processor and configured to receive the second beacon signal and to generate a modulated second beacon signal using a first phase angle and a second phase angle;

wherein the antenna is configured to transmit the first beacon signal and the modulated second beacon signal simultaneously and at the first frequency as a pointing error signal for a ground based receiver, and the antenna is only transmitting device on the satellite to transmit both the first beacon signal and the modulated second beacon signal.

18. The system of claim 17, further comprising:

a receiver in communication with the satellite configured to receive the first beacon signal and the modulated second beacon signal, the receiver including control circuitry configured to;

demodulate the first beacon signal and the modulated second beacon signal; and

determine a pointing error based at least in part on the first beacon signal and the modulated second beacon signal.

19. The system of claim 17, wherein the pointing error signal is defined as a sum of the first beacon signal and the modulated second beacon signal and is represented by the algorithm:

Σ

(t)+Δ

(t)·

exp(jθ

+iπ

)

where Σ

(t) is the first beacon signal, Δ

(t) the second beacon signal, and exp( ) is the base of the natural logarithm, j is an imaginary unit, θ

is an angle about the origin and i is a 0 or a 1 to define the phase shift.