Hybrid RF/optical acquisition and tracking system and method

• US 6,816,112 B1
• Filed: 05/30/2003
• Issued: 11/09/2004
• Est. Priority Date: 05/30/2003
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Chethik, Frank
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US10/452,617
• Time in Patent Office: 529 Days
• Field of Search: 342/357.11, 342/357.14, 342/359, 342/354, 343/725, 343/720, 398/115-117, 398/123, 398/122, 398/121, 398/125
• US Class Current: 342/357.31
• CPC Class Codes: G01S 3/782 Systems for determining direction or deviation from predetermined direction
• CPC Class Codes: H04B 10/118 specially adapted for satellite communication

Abstract

A hybrid optical and millimeter wave beam acquisition and tracking system and method. A host platform includes an INS and a GPS for generating geolocation data, optical and RF receivers, and a common optical/RF aperture. An interface is coupled to the host platform by way of a mechanical gimbal and includes a beamsplitter, an optical gimbal and optical aperture, and an RF aperture. A CPU on the interface includes an optical track error processor for acquiring the optical beam by systematically searching for a focused light spot in a focal plane of the optical receiver, an RF track error processor for outputting gimbal angles of the mechanical gimbal that are derived from the aperture of the RF receiver that are referenced to the inertial navigation system, and a search and track processor that generates an optical gimbal control signal for the optical gimbal and a mechanical gimbal control signal for the mechanical gimbal for tracking the optical and RF beams.

Claims

1. An optical beam acquisition and tracking system comprising:

a host platform comprising an inertial navigation system and a global positioning system for generating geolocation data;

an optical receiver;

a radio frequency (RF) receiver;

a common aperture for use by the optical receiver and RF receiver;

an optical/RF interface coupled to the host platform by way of a mechanical gimbal that comprises;

a beamsplitter for directing optical beam energy along an optical path to the optical receiver and RF energy along an RF path to the RF receiver;

an optical gimbal and optical feed for coupling optical beam energy from the beamsplitter to the optical receiver;

an RF feed for coupling RF energy from the beamsplitter to the RF receiver; and

a central processing unit comprising an optical track error processor for acquiring the optical beam by systematically searching for a focused light spot as it appears in a focal plane of the optical receiver, an RF track error processor for outputting gimbal angles of the mechanical gimbal that are derived from the aperture of the RF receiver and that are referenced to the inertial navigation system, and a search and track processor coupled to the optical track error processor and RF track error processor that generates an optical gimbal control signal for the optical gimbal, and generates a mechanical gimbal control signal for the mechanical gimbal for tracking the optical and RF beams.

2. The system recited in claim 1 wherein the radio frequency receiver comprises a millimeter wave receiver.

3. The system recited in claim 1 wherein the common aperture comprises a conformal window on the platform.

4. The system recited in claim 1 wherein the RF track error processor systematically searches for the received RF beam.

5. The system recited in claim 1 wherein the RF track error processor systematically searches for the received RF beam by performing a scan of an ambiguity region associated with the RF beam.

6. An optical beam acquisition and tracking method comprising the steps of:

providing a host platform that comprises an inertial navigation system and a global positioning system for generating geolocation data, an optical receiver, a radio frequency (RF) receiver, a common optical/RF aperture, and an optical/RF interface coupled to the host platform by way of a mechanical gimbal that comprises a beamsplitter, an optical gimbal and optical feed for coupling optical beam energy from the beamsplitter to the optical receiver, and an RF feed for coupling RF energy from the beamsplitter to the RF receiver;

estimating the location of the platform using the attitude of the host platform derived from the inertial navigation system and the global positioning system;

determining initial ephemeris angles of the mechanical gimbal;

systematically searching an ambiguity region associated with the RF beam until it is acquired;

systematically searching for a focused light spot as it appears in a focal plane of the optical receiver until the optical beam is acquired; and

generating an optical gimbal control signal for the optical gimbal and a mechanical gimbal control signal for the mechanical gimbal for tracking the optical and RF beams.

7. The method recited in claim 6 wherein the step of systematic searching for the received optical beam comprises performing a scan of an ambiguity region associated with the RF beam.

8. The method recited in claim 6 wherein the step of systematic searching for the received optical beam comprises performing a scan of an ambiguity region associated with the RF beam.

9. The method recited in claim 6 wherein the radio frequency receiver comprises a millimeter wave receiver.

10. The method recited in claim 6 wherein the common aperture comprises a conformal window on the platform.