Wide field scanning laser obstacle awareness system

• US 6,650,407 B2
• Filed: 09/04/2001
• Issued: 11/18/2003
• Est. Priority Date: 09/04/2001
• Status: Expired due to Fees

• Current Assignee: Rosemount Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rosemount Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Ray, Mark D., Jamieson, James R.
• Primary Examiner(s): Buczinski, Stephen C.
• Application Number:
  US09/946,058
• Publication Number:
  US 20030046025A1
• Time in Patent Office: 805 Days
• Field of Search: 340/961, 340/963, 340/964, 359/196-226, 356/141.1
• US Class Current: 356/141.1
• CPC Class Codes: B64D 45/08 optical
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G01P 5/26 by measuring the direct influence of the streaming fluid on the properties of a detecting optical wave
• CPC Class Codes: G01S 17/04 Systems determining the presence of a target
• CPC Class Codes: G01S 17/42 Simultaneous measurement of distance and other co-ordinates indirect measurement G01S17/46
• CPC Class Codes: G01S 17/58 Velocity or trajectory determination systems; Sense-of-movement determination systems
• CPC Class Codes: G01S 17/87 Combinations of systems using electromagnetic waves other than radio waves
• CPC Class Codes: G01S 17/88 Lidar systems specially adapted for specific applications
• CPC Class Codes: G01S 17/933 of aircraft or spacecraft
• CPC Class Codes: G01S 7/481 Constructional features, e.g. arrangements of optical elements
• CPC Class Codes: G01S 7/4811 common to transmitter and receiver
• CPC Class Codes: G01S 7/4812 transmitted and received beams following a coaxial path
• CPC Class Codes: G01S 7/4813 Housing arrangements
• CPC Class Codes: G01S 7/4817 relating to scanning
• CPC Class Codes: G01S 7/483 Details of pulse systems
• CPC Class Codes: G01S 7/499 using polarisation effects
• CPC Class Codes: G01S 7/51 Display arrangements
• CPC Class Codes: G02B 26/101 with both horizontal and vertical deflecting means, e.g. raster or XY scanners colour television using laser beams scanning a display screen H04N9/3129

Abstract

A wide field scanning laser obstacle awareness system (LOAS) comprises: a plurality of first optical elements configured to direct a portion of a pulsed laser beam generated by a light source to a light detector, and to direct the pulsed laser beam to a beam expander wherein the pulsed laser beam is expanded; and at least one rotationally operated second optical element for directing the expanded pulsed laser beam from the system with a predetermined pattern scanned azimuthally over a wide field, the at least one rotationally operated second optical element also for receiving reflections of the pulsed laser beam from at least one object along the predetermined pattern and directing them to the laser beam expander wherein the laser beam reflections are focused; the plurality of first optical elements also configured to direct the focused laser beam reflections to the light detector for use in determining the location of the at least one object.

Claims

1. A wide field scanning laser obstacle awareness system (LOAS) for use on-board an aircraft for alerting an operator of obstacles posing a risk of collision with said aircraft, said system comprising:

a light source for generating a pulsed laser beam of light,

a light detector;

a plurality of optical elements for directing said pulsed laser beam from said system with a predetermined pattern scanned azimuthally over a wide field, said plurality of optical elements also for receiving reflections of said pulsed laser beam from at least one object along said predetermined pattern and directing said laser beam reflections to said light detector;

wherein the predetermined pattern includes a variation in elevation of the directed pulsed laser beam in relation to an elevation of the aircraft;

means for determining substantially the azimuth position of the directed pulsed laser beam;

means for determining substantially the elevation of the directed pulsed laser beam;

display apparatus including an image screen for displaying a limited field of view, wherein the wide field of view of the system extends substantially beyond the field of view of the image screen;

processor means coupled to said light detector, display apparatus, azimuth position determining means and elevation determining means for determining the location of the at least one object in range, azimuth and elevation in relation to a flight path of the aircraft, said processor means for driving said display apparatus to display an indication representing the at least one object in range, azimuth and elevation; and

wherein the indication of the at least one object comprises an image of a bar, said bar image disposed vertically at the far left of the screen of the display apparatus when the object location is azimuthally outside the field of view of the display apparatus to the left, and said bar image disposed vertically at the far right of the screen of the display apparatus when the object location is azimuthally outside the field of view of the display apparatus to the right.

2. The system of claim 1 wherein the display apparatus comprises a multi-functional display.

3. The system of claim 1 wherein the indication of the at least one object is overlayed with an existing image on the screen of the display apparatus.

4. The system of claim 1 wherein the bar image is controlled to change color and height based on the risk of collision with the aircraft posed by the object represented thereby.

5. The system of claim 4 wherein the bar image is controlled to change color based on the range of the object to the aircraft in relation to the flight path thereof.

6. The system of claim 4 wherein the bar image is controlled to change height based on the relative height of the object in relation to the elevation of the aircraft.

7. A scanning laser obstacle awareness system (LOAS) comprising:

a light source for generating a pulsed laser beam of light,

a light detector;

a scan head remotely located from said light source and light detector;

at least one first optical element configured to direct said generated pulsed laser beam over a first fiber optic cable to said remote scan head;

said scan head including at least one second optical element for directing said pulsed laser beam from said scan head with a predetermined scan pattern, said at least one second optical element also for receiving reflections of said pulsed laser beam from at least one object along said predetermined scan pattern and directing said laser beam reflections to a second fiber optic cable over which said laser beam reflections are returned to said remote light detector for use in determining the location of said at least one object.

8. The system of claim 7 wherein the at least one second optical element being rotated in azimuth by the scan head to scan the predetermined scan pattern over an azimuth field.

9. The system of claim 7 wherein the at least one second optical element being rotated in elevation by the scan head to scan the predetermined scan pattern over an elevation field.

10. The system of claim 7 including a plurality of scan heads remotely located from the light source and light detector;

wherein light is coupled selectively between the at least one first optical element and the plurality of scan heads along a corresponding plurality of first fiber optic cables.

11. The system of claim 10 wherein the at least one first optical element includes an optical switch controllable to couple light between the light source and a selected scan head of said plurality along a corresponding first fiber optic cable.

12. The system of claim 11 wherein the optical switch comprises a flip mirror operated to rotate about at least one axis.

13. The system of claim 11 wherein the optical switch is fabricated using MEMS techniques.

14. The system of claim 10 wherein each scan head of said plurality for receiving reflections of the pulsed laser beam scanned thereby and for directing said laser beam reflections along a corresponding second fiber optic cable to the remote light detector, wherein said laser beam reflections are received by each scan head of the plurality and returned to said remote light detector over the second fiber optic cable corresponding thereto.

15. The system of claim 10 wherein the LOAS is disposed on-board an aircraft;

wherein the light source, the light detector and at least one first optical element are disposed at a first location of the aircraft and the plurality of scan heads are distributed at a corresponding plurality of second locations along the surface of the aircraft remote from said first location; and

wherein each scan head for directing light therefrom at the predetermined scan pattern of the at least one optical element thereof.

16. The system of claim 7 wherein the at least one second optical element includes a laser beam expander for expanding the pulsed laser beam prior to being directed from the scan head with the predetermined pattern.

17. The system of claim 16 wherein the laser beam expander is configured in the scan head to receive and direct the laser beam reflections to the second fiber optic cable.

18. The system of claim 7 wherein the first and second fiber optic cables are part of a common fiber optic cable.

19. A wide field scanning laser obstacle awareness system (LOAS) for use on-board an aircraft for alerting an operator of obstacles posing a risk of collision with said aircraft, said system comprising:

a light source for generating a pulsed laser beam of light,

a light detector;

a plurality of optical elements for directing said pulsed laser beam from said system with a predetermined pattern scanned azimuthally over a wide field, said plurality of optical elements also for receiving reflections of said pulsed laser beam from at least one object along said predetermined pattern and directing said laser beam reflections to said light detector;

wherein the predetermined pattern includes a variation in elevation of the directed pulsed laser beam in relation to an elevation of the aircraft;

means for determining substantially the azimuth position of the directed pulsed laser beam;

means for determining substantially the elevation of the directed pulsed laser beam;

display apparatus comprising a panel of at least one row and at least one column of light indicators; and

processor means coupled to said light detector, display apparatus, azimuth position determining means and elevation determining means for determining the location of the at least one object in range, azimuth and elevation in relation to a flight path of the aircraft, said processor means for driving said light indicators of the display apparatus to represent a location of the at least one object in azimuth and elevation.

20. The system of claim 19 wherein the light indicators are controlled to change color to indicate the risk of collision of the at least one object with the aircraft.

21. The system of claim 19 wherein the light indicators are controlled to change color to indicate the range of the at least one object to the aircraft.

22. The system of claim 19 wherein the light indicators comprise diodes operative to emit light of different colors.