WO2001075506A1 - Beam steering optical arrangement using risley prisms with surface contours for aberration correction - Google Patents

Beam steering optical arrangement using risley prisms with surface contours for aberration correction Download PDF

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Publication number
WO2001075506A1
WO2001075506A1 PCT/US2000/008506 US0008506W WO0175506A1 WO 2001075506 A1 WO2001075506 A1 WO 2001075506A1 US 0008506 W US0008506 W US 0008506W WO 0175506 A1 WO0175506 A1 WO 0175506A1
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WO
WIPO (PCT)
Prior art keywords
prism
optical
optical axis
angle
prisms
Prior art date
Application number
PCT/US2000/008506
Other languages
French (fr)
Inventor
Scott W. Sparrold
James P. Mills
Richard A. Paiva
Thomas D. Arndt
Kenneth S. Ellis
David J. Knapp
Original Assignee
Raytheon Company
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Raytheon Company filed Critical Raytheon Company
Priority to PCT/US2000/008506 priority Critical patent/WO2001075506A1/en
Priority to EP00921538A priority patent/EP1256028B1/en
Priority to DE60018116T priority patent/DE60018116T2/en
Priority to IL15126900A priority patent/IL151269A0/en
Publication of WO2001075506A1 publication Critical patent/WO2001075506A1/en

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    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/0025—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00 for optical correction, e.g. distorsion, aberration
    • G02B27/0031—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00 for optical correction, e.g. distorsion, aberration for scanning purposes
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B26/00—Optical devices or arrangements for the control of light using movable or deformable optical elements
    • G02B26/08—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
    • G02B26/0875—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light by means of one or more refracting elements
    • G02B26/0883—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light by means of one or more refracting elements the refracting element being a prism
    • G02B26/0891—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light by means of one or more refracting elements the refracting element being a prism forming an optical wedge

Definitions

  • the present invention relates to optical systems. More specifically, the present invention relates to beam steering optical arrangements.
  • a compact, high performance optical arrangement with a steerable beam For many applications, there is a need for a compact, high performance optical arrangement with a steerable beam. Such applications include astronomy, medicine, weaponry and numerous other commercial, industrial and military applications.
  • beam steering is typically accomplished with a gimbaled arrangement.
  • a lens or optical element is mounted to a gimbal.
  • the gimbal is free to rotate about one to three axes.
  • the optical arrangement may be directed to a desired roll angle to steer the beam as necessary.
  • the need in the art is addressed by the steerable optical arrangement of the present invention.
  • the inventive arrangement includes a first prism mounted for rotation about an optical axis and a second prism mounted for rotation about the optical axis.
  • the first prism and/or the second prism have at least one surface contoured to correct for optical aberration.
  • the first and second prisms are Risley prisms.
  • the illustrative implementation includes a first motor arrangement for rotating the first prism about the optical axis and a second motor arrangement for rotating the second prism about the optical axis.
  • a controller is provided for activating the first and second motors to steer the beam at an angle ⁇ and nod the beam at an angle ⁇ .
  • At least one surface of at least one prism is contoured to correct for astigmatism, coma, trefoil, oblique and/or focus.
  • the contour is effected by laser etching, micro- machining or optical thin-film coating of the prisms in the manner disclosed herein.
  • Fig. 1 is a sectional side view of an optical arrangement constructed in accordance with the teachings of the present invention.
  • Fig. 2 is a simplified diagram of the optical arrangement of Fig. 1 with the front and back prisms being rotated to steer the beam at a nod angle of zero degrees.
  • Fig. 3 is a simplified diagram of the optical arrangement of Fig. 1 with the front and back prisms being rotated to steer the beam 26 at a nod angle of ⁇ degrees.
  • Fig. 4 is a side view of a single wedge utilized in the optical arrangement of the present invention.
  • Fig. 5 is a diagram using vector notation to describe the line-of-sight of the optical arrangement of the present invention.
  • Fig. 6 is a diagram showing side views of the first and second prisms of the present invention.
  • Fig. 7 is a diagram showing side views of the first and second prisms of Fig. 1 with surface contours in accordance with the present teachings.
  • Figs. 8, 9, 10a and 10b are diagrams which illustrate conventions used to facilitate an understanding of the teachings provided herein.
  • Fig. 1 1 is a graph which illustrates that aberrations can be generated with counter- rotating phase plates.
  • Fig. 1 is a sectional side view of an optical arrangement constructed in accordance with the teachings of the present invention.
  • the arrangement 10 includes a housing 12 within which a set of wedge-shaped prisms 14 and 16 are disposed.
  • the housing 12 is secured to a stable frame of reference suitable for a given application.
  • the prisms are Risley prisms.
  • the front and back prisms 14 and 16 are independently rotated by first and second motors 18 and 20 respectively.
  • First and second conic-shaped cylinders 22 and 24 connect the first and second prisms 14 and 16 to the first and second motors 18 and 20, respectively.
  • the rotation of the prisms is effective to steer a seeker line of sight (LOS) beam and thereby change the pointing or roll angle ⁇ (not shown in Fig. 1) and the nod angle ⁇ measured with respect to an optical axis 30.
  • the roll angle ⁇ and the nod angle ⁇ are set by the user via an input device 42 and a control circuit 40.
  • the input device 42 may be a microprocessor, ASIC, or other suitable device.
  • the control circuit 40 drives the motors 18 and 20 to rotate the first and second prisms 14 and 16 to steer a beam 26 to the desired roll and nod angles.
  • the LOS is directed by the prisms 14 and 16 to a spherical lens 32.
  • the spherical lens 32 is part of an objective doublet along with an aspherical lens 34.
  • the spherical lens 32 and the aspherical lens 34 are of conventional design and construction.
  • the aspherical lens 34 directs the LOS 26 along the optical path to an eyepiece consisting of first and second lenses 36 and 38.
  • the eyepiece subsequently directs the field of view to an integrated detector assembly 39 and ultimately to an output device 44.
  • Fig. 2 is a simplified diagram of the optical arrangement of Fig. 1 with the front and back prisms being rotated to steer the LOS 26 at a nod angle of zero degrees.
  • Fig. 3 is a simplified diagram of the optical arrangement of Fig. 1 with the front and back prisms being rotated to steer the LOS 26 at a nod angle of ⁇ degrees. As illustrated in Figs. 2 and 3, and in accordance with the present teachings, the line-of-sight of the optical system is stabilized and steered by counter-rotating the wedges 14 and 16.
  • Fig. 4 is a side view of a single wedge 14 or 16.
  • the following equations relate the wedge angle A, the deviation angle D and index of refraction 'n' as follows. Equation [1] relates deviation angle D and index of refraction (n) to wedge angle A for a single wedge for the case where the angle of incidence at the first surface is zero as illustrated in Fig. 4:
  • D is the deviation angle
  • A is the wedge angle
  • n is the index of refraction
  • a wedge made of germanium having an index of refraction of 4 and a wedge angle of 6.5° yields a deviation angle D of 20°. and a high dispersion (Abbe Number of 100).
  • a wedge made of silicon having an index of refraction of 3.4 and a wedge angle of 8.2° yields a deviation angle D of 20° and a low dispersion (Abbe Number of 225).
  • Fig. 5 is a diagram using vector notation to describe the line-of-sight of the optical arrangement of the present invention. As illustrated in Figs. 4 and 5, to achieve a nod motion, the wedges are counter-rotated equal and opposite directions. With two wedges 14 and 16, the deviation angle of each wedge Di and D 2 are related to the nod angle ⁇ by equation [5] below:
  • Fig 6 is a diagram showing side views of the first and second prisms of the present invention
  • Fig 7 is a diagram showing side views of the first and second prisms of Fig 1 with surface contours in accordance with the present teachings
  • each prism has a wedge or trapezoidal geometry from a side view
  • the first prism 14 has a first surface 13 and a second surface 15
  • the second prism 16 has a first surface 17 and a second surface 19
  • the second surface 15 of the first prism faces the first surface 17 of the second prism 16
  • the second surface 15 of the first prism and the first surface 17 of the second prism 16 (hereinafter the 'correction surfaces') are contoured to correct for optical aberrations such as astigmatism, coma, trefoil, oblique and focus
  • the correction surfaces may be etched in accordance with the surface descriptions provided below using photolithography, laser etching, micro-machining, optical thin- films
  • Figs 8, 9, 10a and 10b are diagrams which illustrate conventions used to facilitate an understanding of the teachings provided herein
  • Table I below is a surface deformation table with provides surface descriptions which may be used to correct for the optical aberrations mentioned above along with tilt or nod.
  • the Zernike terms Z4, Z5, Z7 and Z13 can be generated along with Z3, Z6, Z8 and Z10, respectively, by rotating both plates together.
  • Fig. 1 1 is a graph which illustrates that aberrations can be generated with counter- rotating phase plates.

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Optical Elements Other Than Lenses (AREA)

Abstract

A steerable optical arrangement. The inventive arrangement includes a first prism (14) mounted for rotation about an optical axis (30) and a second prism (16) mounted for rotation about the optical axis. In accordance with the inventive teachings, the first prism and/or the second prism have at least one surface contoured to correct for optical aberration. In the illustrative embodiment, the first and second prisms are Risley prisms. In addition, the illustrative implementation includes a first motor arrangement (18) for rotating the first prism (14) about the optical axis (30) and a second motor arrangement (20) for rotating the second prism (16) about the optical axis. A controller (40) is provided for activating the first and second motors to steer the beam at an angle ζ and nod the beam at an angle υ. At least two surfaces of at least one prism is contoured to correct for astigmatism, coma, trefoil and other non-rotationally symmetric aberration. The contour is effected by laser etching, micro-machining or optical thin-film coating of the prisms in the manner disclosed herein.

Description

BEAM STEERING OPTICAL ARRANGEMENT USING RISLEY PRISMS WITH SURFACE CONTOURS FOR ABERRATION CORRECTION
BACKGROUND OF THE INVENTION
Field of the Invention:
The present invention relates to optical systems. More specifically, the present invention relates to beam steering optical arrangements.
Description of the Related Art:
For many applications, there is a need for a compact, high performance optical arrangement with a steerable beam. Such applications include astronomy, medicine, weaponry and numerous other commercial, industrial and military applications. For such applications, beam steering is typically accomplished with a gimbaled arrangement. Typically, a lens or optical element is mounted to a gimbal. The gimbal is free to rotate about one to three axes. Hence, with a motor, the optical arrangement may be directed to a desired roll angle to steer the beam as necessary.
Unfortunately, the gimbal and the actuators for same add to the cost and complexity of the system. In addition, for certain applications, it is desirable to effect beam steering with a more compact arrangement than would be afforded by a typical gimbaled arrangement.
Moreover, in many optical systems, there is a need to correct for optical aberrations. Such aberrations may result from distortion in an input aperture or from some other element in the optical train. Hence, a need exists in the art for a compact, efficient, high performance optical arrangement with a mechanism for effecting beam steering and aberration correction.
SUMMARY OF THE INVENTION
The need in the art is addressed by the steerable optical arrangement of the present invention. The inventive arrangement includes a first prism mounted for rotation about an optical axis and a second prism mounted for rotation about the optical axis. In accordance with the inventive teachings, the first prism and/or the second prism have at least one surface contoured to correct for optical aberration.
In the illustrative embodiment, the first and second prisms are Risley prisms. In addition, the illustrative implementation includes a first motor arrangement for rotating the first prism about the optical axis and a second motor arrangement for rotating the second prism about the optical axis. A controller is provided for activating the first and second motors to steer the beam at an angle φ and nod the beam at an angle θ.
At least one surface of at least one prism is contoured to correct for astigmatism, coma, trefoil, oblique and/or focus. The contour is effected by laser etching, micro- machining or optical thin-film coating of the prisms in the manner disclosed herein.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a sectional side view of an optical arrangement constructed in accordance with the teachings of the present invention.
Fig. 2 is a simplified diagram of the optical arrangement of Fig. 1 with the front and back prisms being rotated to steer the beam at a nod angle of zero degrees. Fig. 3 is a simplified diagram of the optical arrangement of Fig. 1 with the front and back prisms being rotated to steer the beam 26 at a nod angle of φ degrees.
Fig. 4 is a side view of a single wedge utilized in the optical arrangement of the present invention. Fig. 5 is a diagram using vector notation to describe the line-of-sight of the optical arrangement of the present invention.
Fig. 6 is a diagram showing side views of the first and second prisms of the present invention.
Fig. 7 is a diagram showing side views of the first and second prisms of Fig. 1 with surface contours in accordance with the present teachings.
Figs. 8, 9, 10a and 10b are diagrams which illustrate conventions used to facilitate an understanding of the teachings provided herein.
Fig. 1 1 is a graph which illustrates that aberrations can be generated with counter- rotating phase plates.
DESCRIPTION OF THE INVENTION
Illustrative embodiments and exemplary applications will now be described with reference to the accompanying drawings to disclose the advantageous teachings of the present invention.
While the present invention is described herein with reference to illustrative embodiments for particular applications, it should be understood that the invention is not limited thereto. Those having ordinary skill in the art and access to the teachings provided herein will recognize additional modifications, applications, and embodiments within the scope thereof and additional fields in which the present invention would be of significant utility. Fig. 1 is a sectional side view of an optical arrangement constructed in accordance with the teachings of the present invention. The arrangement 10 includes a housing 12 within which a set of wedge-shaped prisms 14 and 16 are disposed. The housing 12 is secured to a stable frame of reference suitable for a given application. Those skilled in the an will appreciate that the prisms are Risley prisms. The front and back prisms 14 and 16 are independently rotated by first and second motors 18 and 20 respectively. First and second conic-shaped cylinders 22 and 24 connect the first and second prisms 14 and 16 to the first and second motors 18 and 20, respectively.
As discussed more fully below, the rotation of the prisms is effective to steer a seeker line of sight (LOS) beam and thereby change the pointing or roll angle θ (not shown in Fig. 1) and the nod angle φ measured with respect to an optical axis 30. The roll angle θ and the nod angle φ are set by the user via an input device 42 and a control circuit 40. The input device 42 may be a microprocessor, ASIC, or other suitable device. The control circuit 40 drives the motors 18 and 20 to rotate the first and second prisms 14 and 16 to steer a beam 26 to the desired roll and nod angles. The LOS is directed by the prisms 14 and 16 to a spherical lens 32. The spherical lens 32 is part of an objective doublet along with an aspherical lens 34. The spherical lens 32 and the aspherical lens 34 are of conventional design and construction.
The aspherical lens 34 directs the LOS 26 along the optical path to an eyepiece consisting of first and second lenses 36 and 38. The eyepiece subsequently directs the field of view to an integrated detector assembly 39 and ultimately to an output device 44. Fig. 2 is a simplified diagram of the optical arrangement of Fig. 1 with the front and back prisms being rotated to steer the LOS 26 at a nod angle of zero degrees.
Fig. 3 is a simplified diagram of the optical arrangement of Fig. 1 with the front and back prisms being rotated to steer the LOS 26 at a nod angle of φ degrees. As illustrated in Figs. 2 and 3, and in accordance with the present teachings, the line-of-sight of the optical system is stabilized and steered by counter-rotating the wedges 14 and 16.
The roll and nod angles α and φ are related to relative angles of the wedges as follows. Fig. 4 is a side view of a single wedge 14 or 16. The following equations relate the wedge angle A, the deviation angle D and index of refraction 'n' as follows. Equation [1] relates deviation angle D and index of refraction (n) to wedge angle A for a single wedge for the case where the angle of incidence at the first surface is zero as illustrated in Fig. 4:
A = arcsin(sin(φ)/(n- 1 )) [ 1 ]
hence
sin A = (sin(φ)/(n-l)) [2] and (n-1) sin A = sin(φ) [3] therefore φ = arcsin ((n-l)sin A) [4]
where D is the deviation angle, A is the wedge angle, and n is the index of refraction.
Thus, a wedge made of germanium having an index of refraction of 4 and a wedge angle of 6.5° yields a deviation angle D of 20°. and a high dispersion (Abbe Number of 100). Likewise, a wedge made of silicon having an index of refraction of 3.4 and a wedge angle of 8.2° yields a deviation angle D of 20° and a low dispersion (Abbe Number of 225).
Fig. 5 is a diagram using vector notation to describe the line-of-sight of the optical arrangement of the present invention. As illustrated in Figs. 4 and 5, to achieve a nod motion, the wedges are counter-rotated equal and opposite directions. With two wedges 14 and 16, the deviation angle of each wedge Di and D2 are related to the nod angle φ by equation [5] below:
φ = 2 sin θ sin" ((n-1) sin A) [5] where θ is the rational angle of each wedge (in opposite direction)
The relationship between the wedge angles, indices of refraction, wedge roll angles and the nod and roll angles φ and α are disclosed in U S Patent Nos 1,735,108 issued November 10, 1929 to H N Cox entitled OPTICAL ADJUSTING DEVICE, 3,253,525 issued May 31, 1966 to F J Merkel entitled VARIABLE OPTICAL WEDGE, 3,507,565 issued April 21, 1970 to L W Alvarez et al ENTITLED VARIABLE- POWER LENS AND SYSTEM, 3,378,326 to Alvarez and 3,884,548 to issued May 20, 1975 to S L Linder entitled VARIABLE OPTICAL WEDGE FOR IMAGE STABLILIZATION AND OTHER PURPOSES the teachings of which are incorporated herein by reference
Fig 6 is a diagram showing side views of the first and second prisms of the present invention Fig 7 is a diagram showing side views of the first and second prisms of Fig 1 with surface contours in accordance with the present teachings As illustrated in Figs 6 and 7, each prism has a wedge or trapezoidal geometry from a side view The first prism 14 has a first surface 13 and a second surface 15 The second prism 16 has a first surface 17 and a second surface 19 The second surface 15 of the first prism faces the first surface 17 of the second prism 16 In accordance with the present teachings, the second surface 15 of the first prism and the first surface 17 of the second prism 16 (hereinafter the 'correction surfaces') are contoured to correct for optical aberrations such as astigmatism, coma, trefoil, oblique and focus Those skilled in the art will appreciate that the correction surfaces may be etched in accordance with the surface descriptions provided below using photolithography, laser etching, micro-machining, optical thin- films or other any suitable technique known in the art
Figs 8, 9, 10a and 10b are diagrams which illustrate conventions used to facilitate an understanding of the teachings provided herein Table I below is a surface deformation table with provides surface descriptions which may be used to correct for the optical aberrations mentioned above along with tilt or nod. Table I
Figure imgf000008_0001
The Zernike terms Z4, Z5, Z7 and Z13 can be generated along with Z3, Z6, Z8 and Z10, respectively, by rotating both plates together.
Fig. 1 1 is a graph which illustrates that aberrations can be generated with counter- rotating phase plates.
Thus, the present invention has been described herein with reference to a particular embodiment for a particular application. Those having ordinary skill in the art and access to the present teachings will recognize additional modifications applications and embodiments within the scope thereof.
It is therefore intended by the appended claims to cover any and all such applications, modifications and embodiments within the scope of the present invention. Accordingly,
WHAT IS CLAIMED IS:

Claims

1. A steerable optical arrangement comprising: a first prism mounted for rotation about an optical axis and a second prism mounted for rotation about said optical axis, said first prism and/or said second prism having at least one surface contoured to correct for optical aberration.
2. The invention of Claim 1 including first means for rotating said first prism about said optical axis.
3. The invention of Claim 2 further including second means for rotating said second prism about said optical axis.
4. The invention of Claim 3 further including means for controlling said first means and said second means to steer a beam at an angle φ.
5. The invention of Claim 4 further including means for controlling said first means and said second means to nod said beam at an angle θ.
6. The invention of Claim 1 wherein said first prism is a Risley prism.
7. The invention of Claim 6 wherein said second prism is a Risley prism.
8. The invention of Claim 1 wherein said optical aberration is astigmatism.
9. The invention of Claim 1 wherein said optical aberration is coma.
10. The invention of Claim 1 wherein said optical aberration is trefoil. 1 1
11. The invention of Claim 1 wherein said optical aberration is any non- rotationally symmetric aberration.
12. The invention of Claim 1 wherein said optical aberration is focus.
13. The invention of Claim 12 wherein said optical aberration is astigmatism.
14. The invention of Claim 13 wherein said optical aberration is coma.
15. The invention of Claim 14 wherein said optical aberration is trefoil.
16. The invention of Claim 1 including means for controlling the rotation of said first prism relative to said second prism.
17. The invention of Claim 16 wherein said means for controlling includes means for rotating said first prism.
18. The invention of Claim 17 wherein said means for controlling includes means for rotating said second prism.
19. A method for steering and correcting an optical line of sight including the steps of: mounting a first prism for rotation about an optical axis and mounting a second prism for rotation about said optical axis, said first prism and/or said second prism having at least one surface contoured to correct for optical aberration. 12
20. The invention of Claim 19 including the step of rotating said first prism about said optical axis and rotating said second prism about said optical axis to steer said line of sight at an angle φ and to nod said line of sight at an angle θ.
21. The invention of Claim 19 wherein said first prism is a Risley prism.
22. The invention of Claim 21 wherein said second prism is a Risley prism.
23. The invention of Claim 19 wherein said optical aberration is astigmatism.
24. The invention of Claim 19 wherein said optical aberration is coma.
25. The invention of Claim 19 wherein said optical aberration is trefoil.
27. The invention of Claim 19 wherein said optical aberration is focus.
PCT/US2000/008506 2000-03-30 2000-03-30 Beam steering optical arrangement using risley prisms with surface contours for aberration correction WO2001075506A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
PCT/US2000/008506 WO2001075506A1 (en) 2000-03-30 2000-03-30 Beam steering optical arrangement using risley prisms with surface contours for aberration correction
EP00921538A EP1256028B1 (en) 2000-03-30 2000-03-30 Beam steering optical arrangement using risley prisms with surface contours for aberration correction
DE60018116T DE60018116T2 (en) 2000-03-30 2000-03-30 Optical arrangement for beam deflection with surface contorted Risley prisms for correction of aberrations
IL15126900A IL151269A0 (en) 2000-03-30 2000-03-30 Beam steering optical arrangement using risley prisms with surface contours for aberration correction

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DE102004007640A1 (en) * 2003-05-28 2004-12-30 Agilent Technologies, Inc. (n.d.Ges.d.Staates Delaware), Palo Alto Kompaktpräzisionsstrahlmanipulierer
GB2422206A (en) * 2005-01-13 2006-07-19 Exitech Ltd Optical device with controlled variation of working angle for laser micromachining operation
US9285581B2 (en) 2013-07-25 2016-03-15 Quartus Engineering Incorporated Optical scanning devices and systems
US10077971B1 (en) 2008-07-07 2018-09-18 Lockheed Martin Corporation Risley prism line-of-sight control for strapdown missile
WO2019164784A1 (en) 2018-02-21 2019-08-29 American Sterilizer Company Refractive lens array assembly
US20200191821A1 (en) * 2018-12-18 2020-06-18 Thales Compact lidar system

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US4826287A (en) * 1987-01-20 1989-05-02 Hughes Aircraft Company Display system having coma-control plate in relay lens
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Publication number Priority date Publication date Assignee Title
DE102004007640A1 (en) * 2003-05-28 2004-12-30 Agilent Technologies, Inc. (n.d.Ges.d.Staates Delaware), Palo Alto Kompaktpräzisionsstrahlmanipulierer
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GB2422206A (en) * 2005-01-13 2006-07-19 Exitech Ltd Optical device with controlled variation of working angle for laser micromachining operation
US10077971B1 (en) 2008-07-07 2018-09-18 Lockheed Martin Corporation Risley prism line-of-sight control for strapdown missile
US9285581B2 (en) 2013-07-25 2016-03-15 Quartus Engineering Incorporated Optical scanning devices and systems
WO2019164784A1 (en) 2018-02-21 2019-08-29 American Sterilizer Company Refractive lens array assembly
EP3755944A4 (en) * 2018-02-21 2021-11-17 American Sterilizer Company Refractive lens array assembly
US20200191821A1 (en) * 2018-12-18 2020-06-18 Thales Compact lidar system

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DE60018116T2 (en) 2006-05-04
DE60018116D1 (en) 2005-03-17
EP1256028A1 (en) 2002-11-13
EP1256028B1 (en) 2005-02-09

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