This invention relates in general to optical devices, and more particularly, to optical imaging systems.
Infra-red optics has been in use by the military for several years, and commercial applications continue to grow. While most of the military development has concentrated on sensors operating in the 8-12 micron spectral band, the advent of large pixel density “staring” detector arrays using materials such as Indium Antimonide (InSb) requires the use of optics designed specifically for the 3-5 micron spectral band. Since these detectors are cryogenically cooled, it is important to provide imaging optics which match the “cold shield” aperture stop within the cryogenic Dewar assembly. For many of the 3-5 micron sensors in existence today, a popular approach is the use of hybrid reflective/refractive catadioptric imaging optics. These have the advantage of obtaining a long focal length within a relatively small package size. However, they suffer from a central obscuration in the entrance pupil. For shorter focal lengths and larger fields of view, a typical approach is to use a simple imaging objective lens assembly.
It is therefore an object of this invention to provide an improved design for an imager in the 3-5 micron spectral band.
This and other objects of the invention are achieved in one aspect by an optical imager for use in the 3-5 micron spectral band. The imager comprises a large aperture positively-powered first objective lens made of a first material for collecting collimated light, and a slightly negatively-powered second objective lens made of a second material spaced behind the first objective lens to provide a color-corrected intermediate focal plane for the collected light. The imager further includes a relay group of three lenses disposed behind the second objective lens for re-imaging the intermediate focal plane.
Another aspect of the invention involves a method of imaging for use in the 3-5 micron spectral band comprising the steps of collecting collimated light with a large aperture positively-powered first objective lens made of a first material, providing a color-corrected intermediate focal plane for the collected light with a slightly negatively-powered second objective lens made of a second material spaced behind the positively-powered lens, and re-imaging the intermediate focal plane with a relay group of three lenses disposed behind the second objective lens.
The optical imager is an all refractive, “re-imaging” device that allows a long focal length and yet still maintains a small package size. The optical imager provides a fully cold shielded aperture stop, and a projected entrance pupil on the first lens in order to keep size minimal. Diffraction limited resolution as characterized by Modulation Transfer Function (MTF) is achieved by use of a single aspheric surface on the first objective lens element. A further benefit over the typical catadioptric approach is that the all-refractive optics do not suffer from a central obscuration in the entrance pupil. This allows full 100% cold shield efficiency and avoids losses in mid and high frequency MTF that result from the diffraction pattern caused by an obscuration.
Additional advantages and features will become apparent as the subject invention becomes better understood by reference to the following detailed description when considered in conjunction with the accompanying drawings wherein:
Table 1 provides the surface description data, showing the relative location of each lens and the air spacing to the next. The radii of curvature for the surfaces of the last of the three lenses 15-17 in the relay group can be further optimized to have identical values, if desired by the lens manufacturer. Table 2 lists both the material indices of refraction and the aspheric surface coefficients, which generate a rotationally symmetric shape according to the following sag equation:
Where z is the sag of the surface parallel to the optical axis, c is the surface curvature defined as the reciprocal of the radius, h is the radial aperture height about the optical axis, k is the conic constant, and A, B, C, and D are the general aspheric coefficients. Table 3 lists the first order parameters of the lens system, which features a 440 mm focal length (the negative sign indicating an inverted image), speed of F#/4.0, and an overall length slightly less than ten inches. The lens assembly will provide a field of view of at least 1.2° on a typical 640×480 element detector with 28 micron pitch.
It is obvious that many modifications and variations of the present invention are possible in light of the above teachings. For example, if a second, wider field of view is desired in addition to the field of view provided here, this design is amenable to a common approach of inserting a small lens group between the first two lenses #1 and #2, which effectively reduces the focal length of the front end objective and couples with the relay group of lenses 13-15. The wide field group can be switched in and out via a variety of mechanisms common to the art, thus providing a dual field of view capability. It is therefore to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as described.
The invention described herein may be manufactured, used, sold, imported, and/or licensed by or for the Government of the United States of America.