Automated director light system for aerial refueling operations

• US 5,904,729 A
• Filed: 03/04/1997
• Issued: 05/18/1999
• Est. Priority Date: 03/04/1997
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Ruzicka, Dennis E.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US08/810,417
• Time in Patent Office: 805 Days
• Field of Search: 704/3, 704/300, 244/135 R, 244/135 A, 244/161, 348/113, 348/116, 348/117, 340/958
• US Class Current: 701/300
• CPC Class Codes: B64D 39/00 Refuelling during flight filling or emptying fuel tanks B64D37/14

Abstract

A method and apparatus for generating visual information for an operator in a first aircraft and a pilot in a second aircraft regarding the second aircraft'"'"'s position relative to a first aircraft. A 3-D camera system (72) generates a real time 3-D video image of the second aircraft. A selecting device (82) provides selection of a stored geometric model based on the second aircraft type. A display monitor (83) displays the generated real time 3-D video image and the selected geometric model. A matching device (84) matches the displayed geometric model to the displayed real time 3-D video image. A processor (84) determines the position of the second aircraft relative to stored zone information according to the matched geometric model and generates control signals according to the determined second aircraft position. Director lights (88) mounted on the outside of the first aircraft display position information visible to the pilot of the second aircraft according to the generated control signals. The monitor also displays the position of the second aircraft relative to a boom.

Claims

1. A director light apparatus in operative relation to a first aircraft for providing a pilot in a second aircraft visual information regarding the second aircraft'"'"'s position relative to the first aircraft;

said apparatus comprising;

a 3-D camera system for generating a real time 3-D video image of the second aircraft;

a first memory for storing at least one geometric model of at least one aircraft;

a selecting means for selecting a stored geometric model based a the 3-D video image of the second aircraft;

a display device for displaying said generated real time 3-D video image and said selected geometric model;

a matching means for matching the displayed geometric model to said displayed real time 3-D video image;

a second memory for storing predefined zone information;

a processor for determining the position of the second aircraft relative to said stored zone information according to said matched geometric model and generating control signals according to said determined second aircraft position; and

director lights mounted on the outside of the first aircraft for displaying position information visible to the pilot of the second aircraft according to said generated control signals.

2. The apparatus of claim 1, wherein:

said zone information comprises a predefined elevation plane, fore/aft plane and azimuth plane referenced from a predefined point relative to the first aircraft; and

said control signals comprise elevation, range and azimuth signals determined according to said determined second aircraft position relative to said predefined elevation plane, fore/aft plane and azimuth plane, respectively.

3. The apparatus of claim 2, wherein:

said director lights comprise an elevation light bar array, a fore/aft lightbar array and an approach lightbar array;

said elevation light bar array illuminates according to said generated elevation signals; and

said fore/aft lightbar array and approach lightbar array illuminate according to said generated range signals.

4. The apparatus of claim 2, further comprising an image generator for generating:

an elevation lightbar image according to said generated elevation signals;

a fore/aft lightbar image and an approach lightbar image according to said generated range signals; and

and an azimuth lightbar image according to said generated azimuth signals on said display device.

5. The apparatus of claim 1, wherein the 3-D camera system comprises two CCD cameras mounted to the first aircraft for viewing the airspace below and aft of a predetermined point a the bottom of the first aircraft.

6. The apparatus of claim 1, wherein said matching means comprises a user interactive device for matching the displayed geometric model to said displayed real time 3-D video image.

7. A method for generating visual information from a first aircraft to a pilot in a second aircraft regarding the second aircraft'"'"'s position relative to the first aircraft;

said method comprising;

generating a real time 3-D video image of the second aircraft;

storing at least one geometric model of at least one aircraft;

selecting a stored geometric model according to the 3-D video image of the second aircraft;

displaying said generated real time 3-D video image and said selected geometric model on a display device within the first aircraft;

matching the displayed geometric model to said displayed real time 3-D video image;

storing predefined zone information;

determining the position of said second aircraft relative to said stored zone information according to said matched geometric model;

generating control signals according to said determined second aircraft position; and

displaying position information visible to the pilot of the second aircraft and an operator within the first aircraft according to said generated control signals.

8. The method of claim 7, wherein:

said zone information comprises a predefined elevation plane, fore/aft plane and azimuth plane referenced from a predefined point relative to the first aircraft; and

said control signals comprise elevation, range and azimuth signals determined according to said determined second aircraft position relative to said predefined elevation plane, fore/aft plane and azimuth plane, respectively.

9. The method of claim 8, further comprising:

generating an elevation lightbar image according to said generated elevation signals, a fore/aft lightbar image and an approach lightbar image according to said generated range signals and an azimuth lightbar image according to said generated azimuth signals a said display device.