System for referencing a direction of an output beam

• US 5,808,732 A
• Filed: 12/20/1996
• Issued: 09/15/1998
• Est. Priority Date: 12/20/1996
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Williams, Samuel George Llewelyn
• Primary Examiner(s): Hellner, Mark
• Application Number:
  US08/773,622
• Time in Patent Office: 634 Days
• Field of Search: 356/139.01, 356/139.03, 356/141.5, 244/171
• US Class Current: 356/139.01
• CPC Class Codes: B64G 1/66 Arrangements or adaptations of apparatus or instruments, not otherwise provided for
• CPC Class Codes: G01C 21/025 with the use of startrackers
• CPC Class Codes: G01S 19/14 specially adapted for specific applications
• CPC Class Codes: G01S 19/53 Determining attitude
• CPC Class Codes: G01S 3/7867 Star trackers navigation using star trackers G01C21/025

Abstract

A system for precisely determining directionality of an output beam includes a beam source and a body position identifier facing opposite directions, with a grating rhomb positioned to provide an attenuated sample beam from the beam source into the oppositely directed body positioned identifier. In the preferred embodiment, the beam source is a pulsed laser source and the body position identifier is a star tracker for forming a stellar map. The grating rhomb includes first and second grating members. The first grating member extends across the optical path of the output beam and has a geometry to diffract a minor portion of the output beam intensity while passing a major portion of the output beam for continued propagation in a first direction. The second grating member is positioned to traverse the field of view of the body position identifier. In the preferred embodiment, the first grating member traverses the optical axis of the output beam and the second grating member is at the intersection of the optical axis of the body position identifier and the optical axis of the diffracted sample beam from the first grating member. The system also includes an auto-collimator that is used to monitor the orientation of the two grating members. When used in a space application, the system also includes a Global Positioning System receiver.

Claims

1. A system for precisely determining a direction of a beam comprising:

a beam source positioned to direct an output beam along an optical path in a first direction;

a body position identifier having a generally fixed optical line of sight in a second direction substantially opposite to said first direction, said body position identifier having a detector responsive to optical signals within a field of view of said body position identifier;

a first grating member extending across said optical path of said output beam, said grating member having a geometry to diffract a minor portion of output beam intensity while passing a major portion of said output beam intensity for continued propagation in said first direction, said diffracted minor portion forming a sample beam; and

a second grating member positioned within said field of view of said body position identifier and within a path of said sample beam, said second grating member being generally transparent to incoming optical signals incoming from a side of said second grating member opposite to said body position identifier, said second grating member having a geometry to diffract a portion of sample beam intensity to said detector of said body position identifier.

2. The system of claim 1 wherein said beam source is a laser source and said first and second grating members form a grating rhomb.

3. The system of claim 1 wherein said first grating member includes a first transparent substrate and a first surface layer having a first grating, said second grating member including a second transparent substrate and a second surface layer having a second grating.

4. The system of claim 3 wherein said first surface layer is on a side of said first transparent substrate proximate to said beam source and wherein said second surface layer is on a side of said second transparent substrate proximate to each of said first grating member and said body position identifier, whereby said sample beam energy which reaches said detector is beam energy reflected at each of said first and second grating members.

5. The system of claim 3 wherein said first surface layer is on a side of said first transparent substrate opposite to said beam source and wherein said second surface layer is on a side of said second transparent substrate opposite to each of said first grating member and said body position identifier, whereby said sample beam energy which reaches said detector is beam energy transmitted and redirected through each of said first and second gratings.

6. The system of claim 1 further comprising a spacecraft housing, each of said beam source, body position identifier and said first and second grating members being contained within said spacecraft housing.

7. The system of claim 6 wherein said body position identifier is a star tracker for forming a stellar map in response to said optical signals within said field of view, said line of sight of said star tracker being directed to image stars, said star tracker and said portion of said sample beam intensity that is diffracted to said detector having generally coincident optical axes.

8. The system of claim 7 further comprising a Global Positioning System (GPS) receiver fixed to said spacecraft housing, each of said GPS receiver and said detector of said star tracker having an input to a signal processor for determining the attitude of said spacecraft housing and the direction of said output beam.

9. The system of claim 1 further comprising an auto-collimator means for monitoring the orientation of said first grating member to said second grating member.

10. A system for precisely determining a direction of a beam comprising:

a star tracker having a first optical axis and a field of view and having a detector for forming star position data in response to light from celestial bodies within said field of view;

beam source means for projecting an output beam having a second optical axis generally parallel to said first optical axis, said beam source means and said star tracker being directed in generally opposite directions;

first grating means along said first optical axis for diffracting a minor portion of beam energy while allowing a major portion to propagate therethrough, said minor portion defining a sample beam, said first grating means having a grating geometry to direct said sample beam to intersect said field of view of said star tracker, said sample beam having a third optical axis;

second grating means generally at an intersection of said sample beam and said field of view of said star tracker for diffracting a minor portion of beam energy of said sample beam toward said star tracker while allowing at least a major portion of light from said celestial bodies within said field of view to propagate therethrough, said minor portion defining an attenuated sample beam; and

processing means for determining an orientation of said second optical axis of said output beam to said star position data.

11. The system of claim 10 further comprising a GPS receiver connected to said processing means for determining a position of said beam source means relative to earth.

12. The system of claim 10 wherein said first and second grating means define a grating rhomb which provides attenuation of said output beam by a factor within the range of 0.5 to 10^-12.

13. The system of claim 10 wherein said second grating means is at an intersection of said third optical axis of said sample beam and said first optical axis of said star tracker.

14. The system of claim 10 wherein said first grating means traverses a beam path of said output beam and said second grating means traverses a beam path of said sample beam.

15. A system for precisely determining a direction of a laser beam for an altimeter determination comprising:

a laser source defining a beam path for an output beam;

imaging means for forming a map of a stellar region, said imaging means facing in a direction generally opposite to said beam path; and

first and second grating members having generally parallel grating surfaces, said first grating member traversing said beam path and said second grating member traversing a field of view of said imaging means, said grating members being largely transmissive while diverting a portion of laser energy of said laser source, said grating members being oriented with respect to each other and said laser source and imaging means such that a sample portion of said laser energy from said laser source is diffracted and directed to said imaging means with a centroid of said sample portion being representative of a centroid of said output beam.

16. The system of claim 15 wherein said imaging means is a star tracker and each of said grating members is a low efficiency member with respect to diffracting said beam energy.

17. The system of claim 15 further comprising a GPS receiver and processing means connected to said GPS receiver for determining a position of said laser source in space.

18. The system of claim 15 further comprising an auto-collimator for monitoring said parallel relationship of said first and second grating surfaces.