Large-focal-ratio wide-field off-axis three-mirror optical system with real entrance pupil
Technical Field
The invention relates to the field of detection of space cameras and spectrograph photographing lenses, in particular to a large-focal-ratio wide-field off-axis three-mirror optical system with a real entrance pupil.
Background
In the detection of a space camera and a spectrograph camera lens, a collimator optical system with a wide field of view and a large focal ratio is required for testing the imaging quality of the space camera and the spectrograph camera lens, and the entrance pupils of the space camera and the spectrograph camera lens need to be matched with the exit pupil surface of a detection optical system, so that the detection optical system needs to have a real entrance pupil.
The off-axis three-mirror optical imaging system has the characteristics of simple structure, no blocking, wide field of view, no dispersion, good image quality, compact structure and the like, can realize high resolution and high energy utilization rate, is increasingly applied to the field of space-to-ground imaging observation such as space cameras, imaging spectrometers and the like, and achieves rapid development.
Usually, the aperture diaphragm of the off-axis three-reflection optical system is positioned on the primary mirror or the secondary mirror, and the actual entrance pupil of the optical system is positioned in the detection light path, so that the accurate matching with the entrance pupil surfaces of the space camera and the spectrograph photographing mirror cannot be realized.
The prior art which is relatively close to the invention is an optical system which is shown in Korsch, D.Antimatic Three-mirror telescope, appl.Opt.16 #8(1977) and Cook, L.G.three-mirror and antislag mat used off-axis in the field, Proc SPIE 183, 207-; the field of view of the optical system described in Cook, l.g. text can be up to 2-4 °. The two diaphragms are positioned on the primary mirror, and have no real entrance pupil, so that the accurate matching of the entrance pupil surfaces of the detected space camera and the spectrometer camera cannot be realized.
Disclosure of Invention
Aiming at the defects in the prior art, the invention aims to provide an off-axis three-mirror optical system with a large focal ratio and a real entrance pupil; the optical system has a real entrance pupil, the focal ratio of the optical system is more than 12, the design field of view is 2 degrees multiplied by 2 degrees, and the wavefront quality of the optical system is better than RMS 1/40.
The technical scheme adopted by the invention for solving the technical problem is as follows:
a large focal ratio off-axis three-mirror optical system with a real entrance pupil comprises a diaphragm, a primary mirror, a secondary mirror, a third reflector (three mirrors for short) and a focal plane, and is characterized in that the real diaphragm is arranged in front of the primary mirror, the distance between the real diaphragm and the primary mirror is larger than the distance between the real diaphragm and the primary mirror, and the real entrance pupil of the off-axis three-mirror optical system is formed; the curvature radius R1 of the primary mirror, the curvature radius R2 of the secondary mirror and the third mirror adopt a convex mirror, and the vertex curvature radius R3 of the convex mirror approximately meets the condition of a flat image field, namely 1/R1+1/R3= 1/R2.
The invention simultaneously adopts a mode of combining the caliber off-axis and the view field off-axis, and realizes that the secondary mirror is in an axisymmetric structure by reasonably selecting the aperture off-axis quantity and the view field off-axis; the optical axes of the primary mirror and the third reflector are coaxial with the secondary mirror, so that the difficulty in assembling and adjusting the optical system is reduced.
The invention further optimizes that:
the primary mirror adopts a concave off-axis hyperboloid primary mirror with positive focal power; an off-axis hyperboloid primary mirror with a high order term of order 4 is recommended.
The secondary mirror adopts a convex negative focal power axial symmetry paraboloid secondary mirror; an axisymmetric parabolic mirror is recommended.
The third reflector (three reflectors for short) adopts a concave off-axis ellipsoidal reflector containing a 4 th-order high-order term.
The distance between the real diaphragm and the primary mirror is larger than the interval between the primary mirror and the secondary mirror.
The distance L1 between the real diaphragm and the primary mirror is greater than the distance L2 between the primary mirror and the secondary mirror.
The entrance pupil diameter of the large-focal-ratio off-axis three-mirror optical system with the real entrance pupil is 350mm, the optical field of view is 2 degrees multiplied by 2 degrees, and the focal ratio of the optical system is F13.8.
The primary mirror is a circular aperture, and the aperture is off-axis 327 mm;
the secondary mirror is a circular aperture and is of an axisymmetric structure;
the third reflector is a square aperture, and the aperture is 326mm away from the axis.
The aperture of the entrance pupil diaphragm is 486.6mm, the field of view in the Y direction is 3 degrees, the field of view in the X-axis direction is-1 to +1 degrees, the field of view in the Y-axis direction is +3 to +5 degrees, and the focal plane size is 242mm × 242 mm.
The primary mirror, the secondary mirror and the third mirror share an optical central shaft.
The curvature radius of the primary mirror is-7475.000 mm, the quadratic coefficient is-2.4751, and the fourth order aspheric coefficient is-2.402 multiplied by 10-13(ii) a The curvature radius of the secondary mirror is-2723.365 mm, and the quadratic coefficient is-1.000;
the curvature radius of the third reflector is-4271.640 mm, the quadratic coefficient is-0.1938, and the fourth order aspheric coefficient is-3.181 multiplied by 10-13。
The distance between the diaphragm and the primary mirror is-2300 mm; the distance between the primary mirror and the secondary mirror is-2070 mm;
the distance between the secondary mirror and the third reflector is-2070 mm; the distance between the three mirrors and the focal plane is-2775.7 mm.
The invention overcomes the defect that the diaphragm is positioned on the primary mirror and has no real entrance pupil, and the accurate matching of the entrance pupil surfaces of the detected space camera and the spectrometer camera can not be realized in the prior art, the optical system has a real entrance pupil, the focal ratio of the optical system is more than 12, the design field of view is 2 degrees multiplied by 2 degrees, and the wavefront quality of the optical system is better than RMS 1/40.
Drawings
FIG. 1 is a schematic diagram of a large focal ratio wide field of view off-axis three-mirror optical system with a real entrance pupil according to the present invention;
FIG. 2 is a top view of the structure of a large focal ratio wide field of view off-axis three-mirror optical system with a real entrance pupil of the present invention;
figure 3 is an RMS wavefront quality of a large focal ratio wide field of view off-axis three-mirror optical system of the present invention with a real entrance pupil.
Detailed Description
Embodiment 1, a large focal ratio off-axis three-mirror optical system with a real entrance pupil, as shown with reference to fig. 1: the whole optical system comprises a diaphragm 1, a primary mirror 2, a secondary mirror 3, a third reflector (three mirrors for short) 4 and a focal plane 5, wherein the primary mirror 1 is a concave off-axis hyperboloid reflector containing 4-order high-order terms, the secondary mirror 2 is a convex axisymmetric paraboloid, and the three mirrors 5 are concave off-axis ellipsoidal reflectors containing 4-order high-order terms.
In the structure, the aperture of an entrance pupil is 350mm, the focal ratio of an optical system is 13.8, the effective field of view is 2 degrees multiplied by 2 degrees, the aperture of the entrance pupil diaphragm in the Y field direction is 486.6mm, the field of view in the Y axis direction of a central field of view is 3 degrees, the field of view in the X axis direction is-1 degrees to +1 degrees, and the field of view in the Y axis direction is +3 degrees to +5 degrees.
In the present embodiment, the real entrance pupil aperture is 486.6mm from the axis; the aperture of the main mirror is phi 484mm, and the aperture is 327mm off-axis; the aperture phi 322mm of the secondary mirror light-transmitting aperture is a rotational axis symmetric structure; the aperture of the light passing through the three mirrors is 517.5mm multiplied by 517.5mm, and the aperture is 326mm off-axis.
In the embodiment, the aperture diaphragm and the primary mirror are separated by-2300 mm; the primary mirror and the secondary mirror are separated by-2070 mm; the secondary mirror and the tertiary mirror are separated by-2070 mm; the three mirrors are spaced-2755.7 mm from the focal plane.
In this embodiment, the curvature radius of the primary mirror is-7475.000 mm, the quadratic coefficient is-2.4751, and the fourth order aspherical coefficient is-2.402 × 10-13(ii) a The curvature radius of the secondary mirror is-2723.365 mm, and the quadratic coefficient is-1.000; the curvature radius of the three mirrors is-4271.640 mm, the quadratic coefficient is-0.1938, and the fourth order aspheric coefficient is-3.181 multiplied by 10-13。
Referring to fig. 3, the RMS wavefront quality of a large focal ratio wide field of view off-axis three-mirror optical system with a real entrance pupil is better than 1/40 wavelengths.