Apparatus suitable for use in orienting aircraft in-flight for refueling or other purposes

• US 4,025,193 A
• Filed: 02/18/1975
• Issued: 05/24/1977
• Est. Priority Date: 02/11/1974
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Robinson, Lawrence W., Texeira, Patrick D., Pond, C. Ray
• Primary Examiner(s): Tubbesing, T.H.
• Assistant Examiner(s): Buczinski, S. C.
• Application Number:
  US05/550,218
• Time in Patent Office: 826 Days
• Field of Search: 356/5, 356/141, 356/152, 244/135 A, 244/77 M
• US Class Current: 356/5.1
• CPC Class Codes: B64D 39/00 Refuelling during flight filling or emptying fuel tanks B64D37/14
• CPC Class Codes: G01S 17/06 Systems determining position data of a target

Abstract

A modulated light beam is projected from a transmitter aircraft toward a receiver aircraft and reflected back toward the receiver aircraft by a retroreflector mounted on the receiver aircraft. The reflected light beam is received by the transmitter aircraft and is focused onto the face of an image dissector tube. The location of the reflected light beam on the face of the tube defines the position of the receiver aircraft in azimuth and elevation with respect to the position of the transmitter aircraft. The range difference between the two aircraft is determined by phase comparing the transmitted light beam with the received light beam. When used for in-flight refueling, further retroreflectors are mounted on a refueling boom and a similar technique is used to determine the exact location of the boom and its associated refueling nozzle. The resultant information is processed by a digital computer and used to either automatically orient the two aircraft, and the boom and nozzle, or create a display(s) suitable for use by one or both aircraft pilots, and the boom operator, to orient the two aircraft, and the boom and nozzle.

Claims

1. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom comprising:

(1) first reflection means mounted on said receiver aircraft for receiving a portion of a transmitted electromagnetic beam and reflecting said portion of said electromagnetic beam back toward the source of said electromagnetic beam as a first reflected beam;

(2) second reflection means mounted on said boom for receiving a portion of a transmitted electromagnetic beam and reflecting said portion of said electromagnetic beam back toward the source of said electromagnetic beam as a second reflected beam; and

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(3) a sensor mounted on said tanker aircraft, said sensor comprising;

(a) electromagnetic transmission means for transmitting an electromagnetic beam in a predetermined direction over a predetermined field of view;

(b) electromagnetic receiving means for receiving the first and second reflected beams of electromagnetic energy reflected by said first and second reflection means mounted on said receiver aircraft and said boom when said receiver aircraft and said boom are in said field of view;

(c) position determining means coupled to said electromagnetic receiving means for determining the positions of said first and second reflected beams in said field of view; and

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(d) ranging means connected to said receiving means and said transmitting means for determining the time difference between transmission of said electromagnetic beam to, and reception of said first reflected beam from said receiver aircraft and, thus, the range between said receiver aircraft and said tanker aircraft.

2. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 1 including display means connected to said position determining means and to said ranging means for displaying the position of said boom and said receiver aircraft with respect to said tanker aircraft, and for displaying the range and range rates between said two aircraft.

3. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 2 wherein the frequency of said electromagnetic beam is within the light spectrum between 0.2 and 20 microns wavelength.

4. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 3 wherein said first and second reflection means are retroreflectors.

5. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 4 wherein said ranging means includes:

phase detecting means suitable for detecting the phase difference between said transmitted electromagnetic beam and said first reflected beam; and

digital counting means connected to said phase detecting means for providing a digital pulse count related to the distance between said receiver and tanker aircraft, said digital counting means being started at a predetermined phase point in said transmitted beam and stopped when a related phase point in said received beam occurs.

6. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 5 wherein said display means includes a first display associated with said receiver aircraft and a second display associated with said tanker aircraft.

7. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 6 wherein said transmission means comprises a light source, a driver connected to said light source for modulating the light emitted by said light source, and projecting optics suitable for receiving the light generated by said light source and projecting said light outwardly as a light beam.

8. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 7 wherein said receiving means comprises receiving optics suitable for receiving said received beams and wherein said position determining means comprises an image dissector tube, said image dissector tube being mounted such that said reflected beams received by said receiving optics are imaged onto the face of the image dissector tube.

9. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 8 including:

a scan mirror mounted so as to intersect the light beam output of said projecting optics and transmit said light beam output from said tanker aircraft in a scanning manner, said scan mirror also being mounted so as to intersect said received light beams and direct said beams toward said receiving optics; and

electromechanical means connected to said scan mirror for moving said scan mirror in a scanning manner over said field of view.

10. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 1 wherein said transmission means comprises a light source, a driver connected to said light source for modulating the light emitted by said light source, and projecting optics suitable for receiving the light generated by said light source and projecting said light outwardly as a light beam.

11. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 10 wherein said receiving means comprises receiving optics suitable for receiving said received beams and wherein said position determining means comprises an image dissector tube, said image dissector tube being mounted such that said reflected beams received by said receiving optics are imaged onto the face of the image dissector tube.

12. Apparatus suitable for use in in-flight refueling a receiver aircraft by a tanker aircraft via a refueling boom as claimed in claim 11 including:

a scan mirror mounted so as to intersect the light beam output of said projecting optics and transmit said light beam output from said tanker aircraft in a scanning manner, said scan mirror also being mounted so as to intersect said received light beams and direct said beams toward said receiving optics; and

electromechanical means connected to said scan mirror for moving said scan mirror in a scanning manner over said field of view.

13. Apparatus suitable for use in in-flight orienting a first aircraft with respect to a second aircraft comprising:

(1) a plurality of retroreflectors, mounted on said first aircraft in a predetermined array, for receiving portions of a transmitted electromagnetic beam and reflecting the portions of said electromagnetic beam received by each of said retroreflectors back toward the source of said electromagnetic beam;

(2) a sensor mounted on said second aircraft, said sensor comprising;

(a) electromagnetic transmission means for transmitting an electromagnetic beam, having a frequency lying in the light spectrum, in a predetermined direction over a predetermined field of view, said electromagnetic transmission means including;

(i) a light source;

(ii) a driver connected to said light source for modulating the light emitted by said light source;

(iii) projecting optics mounted so as to receive the light generated by said light source and project said light outwardly as a light beam;

(iv) a scan mirror mounted so as to intersect the light beam projected by said projecting optics and transmit said light beam outwardly from said second aircraft in a scanning manner, said scan mirror also being mounted so as to intersect and redirect the portions of said electromagnetic beam reflected by said retroreflectors; and

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(v) electromechanical means connected to said scan mirror for moving said scan mirror such that said outwardly transmitted light beam scans said field of view;

(b) electromagnetic receiving means for receiving the portions of said transmitted electromagnetic beam reflected by said retroreflectors mounted on said first aircraft when said first aircraft is in said field of view, said electromagnetic receiving means including receiving optics positioned so as to receive the portions of said electromagnetic beam reflected by said retroreflectors and redirected by said scan mirror;

(c) position determining means coupled to said electromagnetic receiving means for determining the position of said portions of said transmitted electromagnetic beam reflected by said retroreflectors, said position determining means including an image dissector tube, said image dissector tube being mounted such that said portions of said electromagnetic beam reflected by said retroreflectors and received by said receiving optics is imaged onto the face of said image dissector tube; and

(d) ranging means connected to said electromagnetic receiving means and said electromagnetic transmitting means for determining the time difference between the transmission of said transmitted electromagnetic beam and the reception of said portions of said transmitted electromagnetic beam reflected by said retroreflectors and, thus, the range between said first aircraft and said second aircraft, said ranging means including;

(i) phase detecting means suitable for detecting the phase difference between said transmitted electromagnetic beam and said portions of said electromagnetic beam reflected by said retroreflectors; and

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(ii) digital counting means connected to said phase detecting means for providing a digital pulse count related to the range between said first and second aircraft, said digital counting means being started at a predetermined phase point in said transmitted beam cycle and stopped when a related phase point in the cycle of said reflected beams occurs; and

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(3) display means mounted in said second aircraft and connected to said position determining means and said ranging means for displaying the position of said first aircraft with respect to said second aircraft, and the range between said first aircraft and said second aircraft.