Satellite orientation detection system

• US 5,258,764 A
• Filed: 09/26/1991
• Issued: 11/02/1993
• Est. Priority Date: 09/26/1991
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Original Assignee: Santa Barbara Research Center (Rtx Corporation)
• Inventors: Malinowski, Frank R.
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US07/766,695
• Time in Patent Office: 768 Days
• Field of Search: 342/352, 342/355, 342/361, 342/362, 342/365, 342/77, 342/359, 342/363
• US Class Current: 342/359
• CPC Class Codes: H01Q 1/1257 using the received signal strength
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 3/14 for varying the relative position of primary active element and a refracting or diffracting device

Abstract

A satellite orientation detection system disposed to detect the pointing orientation of a geosynchronous satellite (10) relative to a reference location on the earth. The present invention is also capable of ascertaining the angular orientation of a longitudinal axis of the satellite (10) relative to a defined axis on the surface of the earth. A ground station (20) is included for transmitting a first linearly polarized and a second circularly polarized electromagnetic reference beam. The present system also includes a receive antenna (28) coupled to the satellite (10) for receiving the first and second reference beams and for generating an antenna-beam pattern P1 and P2 disposed to rotate about a reference axis A. A rotating polarizer arrangement (44), aligned with the receive antenna (28), periodically varies the portion of the linearly polarized energy within the first reference beam transmitted thereby. The present invention further includes a first network (54) for detecting the intensity of the received portion of said first reference beam and for generating a roll error signal indicative of the angle between the longitudinal axis and the first polarization direction in response thereto. A second network (80) generates pitch and yaw pointing error signals in response to time variation in the intensity of the received portion of the second reference beam.

Claims

1. A system for detecting the pointing and roll orientation of a geosynchronous satellite relative to a reference location on the earth, said satellite having a pointing direction and a longitudinal axis, comprising:

a ground station for transmitting first and second reference beams of electromagnetic energy, said first beam being linearly polarized along a first axis and said second beam being circularly polarized;

a receive antenna, coupled to said satellite, for receiving said first and second reference beams and for generating an antenna-beam pattern which rotates about a reference axis;

rotating polarizer means, aligned with said receive antenna, for periodically varying the portion of said linearly polarized energy within said first reference beam transmitted thereby and for transmitting said circularly polarized second reference beam;

first means for detecting the intensity of said received portion of said first reference beam and for generating a roll error signal indicative of the angle between said longitudinal axis and said first axis in response thereto; and

second means for generating pitch and yaw error signals indicative of the orientation of said reference axis relative to said reference location in response to time variation in the intensity of said received portion of said second reference beam.

2. The orientation detection system of claim 1 wherein said ground station includes means for modulating said first reference beam with a first modulating signal of a first frequency and means for modulating said second reference beam with a second modulating signal of a second frequency.

3. The orientation detection system of claim 2 wherein said rotating polarizer means includes a polarizing disk which transmits substantially all of said first reference beam incident thereon when oriented in alignment with said first axis, and which transmits substantially none of said first reference beam incident thereon when oriented approximately ninety degrees from said first axis.

4. The orientation detection system of claim 3 wherein said receive antenna means further includes a scan modulating disk aligned with said polarizing disk for rotating said antenna-beam pattern.

5. The orientation detection system of claim 4 wherein said scan modulating disk is transparent to said first and second reference beams and has a wedge-shaped cross-section along a first axis thereof.

6. The system of claim 5 wherein said scan modulating disk and said polarizing disk rotate about a common axis at an identical angular velocity.

7. The system of claim 1 further including a two-axis pointing mirror coupled to said satellite for adjusting the direction of said reference axis.

8. The orientation detection system of claim 2 wherein said receiving means includes:

an antenna feed and

mixer means for generating a first intermediate frequency signal in response to said received portion of said first reference beam and for generating a second intermediate frequency signal in response to said received portion of said second reference beam.

9. The orientation detection system of claim 8 wherein said first means includes a first intermediate frequency detector for detecting said first intermediate frequency signal and wherein said second means includes a second intermediate frequency detector for detecting said second intermediate frequency signal.

10. The orientation detection system of claim 9 wherein said first means further includes a first low-frequency detector coupled to said first intermediate frequency detector for detecting said first modulating signal, and a second low-frequency detector coupled to said second intermediate frequency detector for detecting said second modulating signal.

11. The orientation system of claim 10 wherein said first means includes means for generating a first scan reference signal indicative of the orientation of said polarizing disk and said second means includes means for generating a second scan reference signal in response to the orientation of said scan modulating disk.

12. The orientation system of claim 11 wherein said first means includes a first sampling circuit for generating a roll error signal response to said detected first modulating signal and to said first scan reference signal.

13. The orientation system of claim 12 wherein said second means includes a second sampling circuit for generating pitch and yaw error signals in response to said detected second modulating signal and to said second scan reference signal.

14. A method for detecting the pointing and roll orientation of a geosynchronous satellite relative to a reference location on the earth, said satellite having a pointing direction and longitudinal axis, comprising the steps of:

a) transmitting first and second reference beams of electromagnetic energy, said first beam being linearly polarized along a first axis and said second beam being circularly polarized;

b) projecting an antenna-beam pattern from said satellite;

c) rotating said antenna-beam pattern about said reference axis;

d) positioning a rotating polarizer coupled to said satellite in alignment with said first and second reference beams;

e) varying the portion of said first reference beam transmitted by said rotating polarizer;

f) receiving said transmitted portions of said first and second reference beams;

g) detecting the intensity of said received portion of said first reference beam and generating a roll error signal indicative of the angle between said longitudinal axis and said first axis in response thereto; and

h) generating pitch and yaw error signals in response to the intensity of said received portion of said second reference beam.