On-orbit reconfigurability of a shaped reflector with feed/reflector defocusing and reflector gimballing

• US 6,031,502 A
• Filed: 11/27/1996
• Issued: 02/29/2000
• Est. Priority Date: 11/27/1996
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Original Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Inventors: Dixon, Cynthia A., Estevez, Miguel A., Ramanujam, Parthasarathy, Fermelia, Louis R.
• Primary Examiner(s): Wimer, Michael C.
• Application Number:
  US08/753,660
• Time in Patent Office: 1,189 Days
• Field of Search: 343/781 P, 343/761, 343/837, 343/839, 343/840, 343/764, 343/781 R
• US Class Current: 343/761
• CPC Class Codes: H01Q 1/18 Means for stabilising antennas on an unstable platform
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 15/141 Apparatus or processes specially adapted for manufacturing reflecting surfaces
• CPC Class Codes: H01Q 3/16 for varying relative position of primary active element and a reflecting device
• CPC Class Codes: H01Q 3/18 wherein the primary active element is movable and the reflecting device is fixed
• CPC Class Codes: H01Q 3/20 wherein the primary active element is fixed and the reflecting device is movable

Abstract

A system and method for changing the radiation pattern of an antenna assembly of a satellite in orbit is provided. The antenna assembly includes a reflector antenna fed by a feed assembly. The reflector antenna transmits and receives signals within a radiation pattern. The reflector antenna and the feed assembly are movably mounted to a sliding mechanism so that they can be displaced with respect to one another. The displacement causes defocusing as the reflector antenna is displaced from the focus point. The defocusing causes the radiation pattern to become more compact or broadened. Thus, the radiation pattern of the satellite provided with a single reflector antenna and a single feed element may be changed while the satellite is in orbit. The system and method include gimballing the reflector antenna to steer the radiation pattern.

Claims

1. A satellite positioned in orbit above the Earth for transmitting a radiation pattern of electromagnetic energy to the Earth, the satellite comprising:

a sliding mechanism;

a shaped reflector for transmitting a shaped radiation pattern of electromagnetic energy to the Earth; and

a feed assembly positioned at a given distance from the shaped reflector for illuminating the shaped reflector with electromagnetic energy;

wherein the shaped reflector transmits the electromagnetic energy received from the feed assembly in the radiation pattern to the Earth;

wherein at least one of the shaped reflector and the feed assembly is movably mounted to the sliding mechanism to vary the given distance between the shaped reflector and the feed assembly for defocusing the shaped reflector and the feed assembly thereby changing the radiation pattern of electromagnetic energy transmitted to the Earth while the satellite is in orbit above the Earth.

2. The satellite of claim 1 further comprising:

a gimballing mechanism for tilting and rotating the shaped reflector to steer the radiation pattern.

3. The satellite of claim 1 wherein the feed assembly comprises:

a sub-reflector; and

a feed element for illuminating the sub-reflector with electromagnetic energy;

wherein the sub-reflector illuminates the shaped reflector with the electromagnetic energy received from the feed element.

4. The satellite of claim 3 wherein at least one of the sub-reflector and the feed element is movably mounted to the sliding mechanism.

5. The satellite of claim 1 further comprising:

a stepping motor cooperating with the sliding mechanism to move at least one of the shaped reflector and the feed assembly.

6. The satellite of claim 1 wherein the feed assembly is offset from an axis extending through and perpendicular to an origin of the shaped reflector.

7. A method for a satellite positioned in orbit above the Earth for transmitting a radiation pattern of electromagnetic energy to the Earth, wherein the satellite is provided with a feed assembly and a shaped reflector, the method comprising:

positioning the feed assembly at a given distance from the shaped reflector;

illuminating the shaped reflector with electromagnetic energy from the feed assembly;

transmitting the electromagnetic energy from the shaped reflector in a shaped radiation pattern to the Earth; and

displacing at least one of the shaped reflector and the feed assembly to vary the given distance between the shaped reflector and the feed assembly for defocusing the shaped reflector and the feed assembly thereby changing the radiation pattern of electromagnetic energy transmitted to the Earth while the satellite is in orbit above the Earth.

8. The method of claim 7 wherein illuminating the shaped reflector with electromagnetic energy from the feed assembly comprises:

illuminating a sub-reflector with electromagnetic energy from a feed element; and

illuminating the shaped reflector with the electromagnetic energy received by the sub-reflector.

9. The method of claim 8 wherein displacing at least one of the shaped reflector and the feed assembly comprises:

displacing at least one of the shaped reflector, the sub-reflector, and the feed element.

10. The method of claim 7 further comprising:

steering the radiation pattern by tilting and rotating the shaped reflector.

11. A method for a satellite positioned in orbit above the Earth for receiving a radiation pattern of electromagnetic energy from the Earth, wherein the satellite is provided with a feed assembly and a shaped reflector, the method comprising:

positioning the feed assembly at a given distance from the shaped reflector;

receiving electromagnetic energy from the Earth in a radiation pattern with the shaped reflector;

illuminating the feed assembly with the electromagnetic energy received from the shaped reflector; and

displacing at least one of the shaped reflector and the feed assembly to vary the given distance between the shaped reflector and the feed assembly for defocusing the shaped reflector and the feed assembly thereby changing the radiation pattern of electromagnetic energy received from the Earth while the satellite is in orbit above the Earth.

12. The method of claim 11 wherein illuminating the feed assembly with the electromagnetic energy received from the shaped reflector comprises:

illuminating a sub-reflector with electromagnetic energy from the shaped reflector; and

illuminating a feed element with the electromagnetic energy received from the sub-reflector.

13. The method of claim 12 wherein displacing at least one of the shaped reflector and the feed assembly comprises:

displacing at least one of the shaped reflector, the sub-reflector, and the feed element.

14. The method of claim 11 further comprising:

steering the radiation pattern by rotating and tilting the shaped reflector.