System and method for testing optical proximity fuses

Patent metadata

Field	Value
Publication number	US-12553697-B2
Application number	US-202218847747-A
Country	US
Kind code	B2
Filing date	Dec 27, 2022
Priority date	Mar 17, 2022
Publication date	Feb 17, 2026
Grant date	Feb 17, 2026

Abstract

A system ( 10 ) for testing a laser proximity fuse (PF) ( 12 ) by simulating a closing velocity to a target along a line of sight ( 14 ) includes a static spiral surface ( 16 ) and a support arrangement ( 18 ) for supporting the proximity fuse ( 12 ) with the line of sight ( 14 ) directed towards an inside of static spiral surface ( 16 ). A folding mirror ( 20 ) is driven by a drive motor ( 22 ) so as to deflect the line of sight ( 14 ) towards progressively closer regions of static spiral surface, thereby simulating a closing velocity. The system can be miniaturized by employing converging optics ( 24 ). An alternative embodiment employs a shaped rotor ( 32 ) to achieve a similar effect.

First claim

What is claimed is:

1 . A system for testing a laser proximity fuse by simulating a closing velocity to a target along a line of sight, the system comprising:
(a) a static spiral surface; (b) a support arrangement for supporting the proximity fuse with the line of sight directed towards an inside of the static spiral surface; (c) a folding mirror deployed for deflecting the line of sight towards the static spiral surface; and (d) a drive motor deployed for rotating said folding mirror such that the line of sight scans along the static spiral surface, thereby simulating a closing velocity.

2 . The system of claim 1 , wherein said static spiral surface has a curvature corresponding to a segment of an Archimedean spiral.

3 . The system of claim 1 , wherein said static spiral surface has an origin, and wherein said folding mirror is deployed at said origin.

4 . The system of claim 1 , further comprising converging optics deployed between said support arrangement and said folding mirror, said converging optics having a focal length, and wherein all parts of said static spiral surface are deployed at a light path length from said converging optics that is less than said focal length.

5 . The system of claim 1 , wherein said drive motor is an adjustable drive motor configured to rotate at a range of angular speeds effective to simulate closing velocities over a range extending up to at least 100 meters per second.

6 . A method for testing a laser proximity fuse by simulating a closing velocity to a target along a line of sight, the method comprising the steps of:
(a) providing the system of any one of the preceding claims ; (b) deploying the proximity fuse supported by said support arrangement so that a line of sight of the laser is directed towards said folding mirror; (c) actuating the drive motor so as to rotate the folding mirror; and (d) actuating the proximity fuse synchronously with rotation of the drive motor so that the laser scans along said static spiral surface, thereby simulating a closing velocity.

7 . The method of claim 6 , further comprising introducing a visibility-disrupting material or structure between said folding mirror and said static spiral surface.

8 . A system for testing a laser proximity fuse by simulating a closing velocity to a target along a line of sight, the system comprising:
(a) a support arrangement for supporting the proximity fuse with the line of sight directed along an optical axis; (b) a rotor having external surfaces deployed to intersect the optical axis; (c) a drive motor deployed for rotating said rotor to present successive regions of said external surface on said optical axis; and (d) converging optics deployed between said support arrangement and said rotor, said converging optics having a focal length, and wherein said rotor is deployed at a distance from said converging optics that is less than said focal length,
wherein said external surfaces of said rotor are shaped such that, when said rotor rotates, a length of a light path from the proximity fuse to the region of the rotor intersected by the optical axis varies so as to simulate a closing velocity.

9 . The system of claim 8 , wherein said rotor has two-fold rotational symmetry.

Assignees

• Rafael Advanced Defense Systems Ltd

Inventors

• Tibi Dov

Classifications

• G01S17/08

  for measuring distance only (indirect measurement G01S17/46; active triangulation systems G01S17/48) · CPC title

• G01S7/497

  Means for monitoring or calibrating · CPC title

• F42C13/023

  using active distance measurement · CPC title

• F42C13/02

  operated by intensity of light or similar radiation · CPC title

• G01S17/88

  Lidar systems specially adapted for specific applications · CPC title