- •Lens Design Fundamentals
- •Contents
- •Preface to the Second Edition
- •Preface to the First Edition
- •A Special Tribute to Rudolf Kingslake
- •1.1. Relations Between Designer and Factory
- •1.1.1 Spherical versus Aspheric Surfaces
- •1.1.2 Establishment of Thicknesses
- •1.1.3 Antireflection Coatings
- •1.1.4 Cementing
- •1.1.5 Establishing Tolerances
- •1.1.6 Design Tradeoffs
- •1.2. The Design Procedure
- •1.2.1 Sources of a Likely Starting System
- •1.2.2 Lens Evaluation
- •1.2.3 Lens Appraisal
- •1.2.4 System Changes
- •1.3. Optical Materials
- •1.3.1 Optical Glass
- •1.3.2 Infrared Materials
- •1.3.3 Ultraviolet Materials
- •1.3.4 Optical Plastics
- •1.4. Interpolation of Refractive Indices
- •1.4.1 Interpolation of Dispersion Values
- •1.4.2 Temperature Coefficient of Refractive Index
- •1.5. Lens Types to be Considered
- •2.1. Introduction
- •2.1.1 Object and Image
- •2.1.2 The Law of Refraction
- •2.1.3 The Meridional Plane
- •2.1.4 Types of Rays
- •2.1.5 Notation and Sign Conventions
- •2.2. Graphical Ray Tracing
- •2.3. Trigonometrical Ray Tracing at a Spherical Surface
- •2.3.1 Program for a Computer
- •2.4. Some Useful Relations
- •2.4.1 The Spherometer Formula
- •2.4.2 Some Useful Formulas
- •2.4.3 The Intersection Height of Two Spheres
- •2.4.4 The Volume of a Lens
- •2.5. Cemented Doublet Objective
- •2.6. Ray Tracing at a Tilted Surface
- •2.6.1 The Ray Tracing Equations
- •2.6.2 Example of Ray Tracing through a Tilted Surface
- •2.7. Ray Tracing at an Aspheric Surface
- •3.1. Tracing a Paraxial Ray
- •3.1.1 The Standard Paraxial Ray Trace
- •3.1.2 The (y – nu) Method
- •3.1.3 Inverse Procedure
- •3.1.4 Angle Solve and Height Solve Methods
- •3.1.6 Paraxial Ray with All Angles
- •3.1.7 A Paraxial Ray at an Aspheric Surface
- •3.1.9 Matrix Approach to Paraxial Rays
- •3.2. Magnification and the Lagrange Theorem
- •3.2.1 Transverse Magnification
- •3.2.2 Longitudinal Magnification
- •3.3. The Gaussian Optics of a Lens System
- •3.3.1 The Relation between the Principal Planes
- •3.3.2 The Relation between the Two Focal Lengths
- •3.3.3 Lens Power
- •3.3.4 Calculation of Focal Length
- •3.3.5 Conjugate Distance Relationships
- •3.3.6 Nodal Points
- •3.3.7 Optical Center of Lens
- •3.3.8 The Scheimpflug Condition
- •3.4. First-Order Layout of an Optical System
- •3.4.1 A Single Thick Lens
- •3.4.2 A Single Thin Lens
- •3.4.3 A Monocentric Lens
- •3.4.4 Image Shift Caused by a Parallel Plate
- •3.4.5 Lens Bending
- •3.4.6 A Series of Separated Thin Elements
- •3.4.7 Insertion of Thicknesses
- •3.4.8 Two-Lens Systems
- •3.5. Thin-Lens Layout of Zoom Systems
- •3.5.1 Mechanically Compensated Zoom Lenses
- •3.5.2 A Three-Lens Zoom
- •3.5.4 A Four-Lens Optically Compensated Zoom System
- •3.5.5 An Optically Compensated Zoom Enlarger or Printer
- •Endnotes
- •4.1. Introduction
- •4.2. Symmetrical Optical Systems
- •4.3. Aberration Determination Using Ray Trace Data
- •4.3.1 Defocus
- •4.3.2 Spherical Aberration
- •4.3.3 Tangential and Sagittal Astigmatism
- •4.3.4 Tangential and Sagittal Coma
- •4.3.5 Distortion
- •4.3.6 Selection of Rays for Aberration Computation
- •4.3.7 Zonal Aberrations
- •4.3.8 Tangential and Sagittal Zonal Astigmatism
- •4.3.9 Tangential and Sagittal Zonal Coma
- •4.3.10 Higher-Order Contributions
- •4.4. Calculation of Seidel Aberration Coefficients
- •Endnotes
- •5.1. Introduction
- •5.2. Spherochromatism of a Cemented Doublet
- •5.2.4 Secondary Spectrum
- •5.2.5 Spherochromatism
- •5.3. Contribution of a Single Surface to the Primary Chromatic Aberration
- •5.4. Contribution of a Thin Element in a System to the Paraxial Chromatic Aberration
- •5.5. Paraxial Secondary Spectrum
- •5.7.1 Secondary Spectrum of a Dialyte
- •5.7.2 A One-Glass Achromat
- •5.8. Chromatic Aberration Tolerances
- •5.8.1 A Single Lens
- •5.8.2 An Achromat
- •5.9. Chromatic Aberration at Finite Aperture
- •5.9.1 Conrady’s D – d Method of Achromatization
- •5.9.3 Tolerance for the D – d Sum
- •5.9.5 Paraxial D – d for a Thin Element
- •Endnotes
- •6.1. Surface Contribution Formulas
- •6.1.1 The Three Cases of Zero Aberration at a Surface
- •6.1.2 An Aplanatic Single Element
- •6.1.3 Effect of Object Distance on the Spherical Aberration Arising at a Surface
- •6.1.4 Effect of Lens Bending
- •6.1.6 A Two-Lens Minimum Aberration System
- •6.1.7 A Four-Lens Monochromat Objective
- •6.2. Zonal Spherical Aberration
- •6.3. Primary Spherical Aberration
- •6.3.1 At a Single Surface
- •6.3.2 Primary Spherical Aberration of a Thin Lens
- •6.4. The Image Displacement Caused by a Planoparallel Plate
- •6.5. Spherical Aberration Tolerances
- •6.5.1 Primary Aberration
- •6.5.2 Zonal Aberration
- •Endnotes
- •7.1. The Four-Ray Method
- •7.2. A Thin-Lens Predesign
- •7.2.1 Insertion of Thickness
- •7.2.2 Flint-in-Front Solutions
- •7.3. Correction of Zonal Spherical Aberration
- •7.4. Design Of an Apochromatic Objective
- •7.4.1 A Cemented Doublet
- •7.4.2 A Triplet Apochromat
- •7.4.3 Apochromatic Objective with an Air Lens
- •Endnotes
- •8.1. Passage of an Oblique Beam through a Spherical Surface
- •8.1.1 Coma and Astigmatism
- •8.1.2 Principal Ray, Stops, and Pupils
- •8.1.3 Vignetting
- •8.2. Tracing Oblique Meridional Rays
- •8.2.1 The Meridional Ray Plot
- •8.3. Tracing a Skew Ray
- •8.3.1 Transfer Formulas
- •8.3.2 The Angles of Incidence
- •8.3.3 Refraction Equations
- •8.3.4 Transfer to the Next Surface
- •8.3.5 Opening Equations
- •8.3.6 Closing Equations
- •8.3.7 Diapoint Location
- •8.3.8 Example of a Skew-Ray Trace
- •8.4. Graphical Representation of Skew-Ray Aberrations
- •8.4.1 The Sagittal Ray Plot
- •8.4.2 A Spot Diagram
- •8.4.3 Encircled Energy Plot
- •8.4.4 Modulation Transfer Function
- •8.5. Ray Distribution from a Single Zone of a Lens
- •Endnotes
- •9.1. The Optical Sine Theorem
- •9.2. The Abbe Sine Condition
- •9.2.1 Coma for the Three Cases of Zero Spherical Aberration
- •9.3. Offense Against the Sine Condition
- •9.3.1 Solution for Stop Position for a Given OSC
- •9.3.2 Surface Contribution to the OSC
- •9.3.3 Orders of Coma
- •9.3.4 The Coma G Sum
- •9.3.5 Spherical Aberration and OSC
- •9.4. Illustration of Comatic Error
- •Endnotes
- •10.1. Broken-Contact Type
- •10.2. Parallel Air-Space Type
- •10.3. An Aplanatic Cemented Doublet
- •10.4. A Triple Cemented Aplanat
- •10.5. An Aplanat with A Buried Achromatizing Surface
- •10.6. The Matching Principle
- •Endnotes
- •11.1. Astigmatism and the Coddington Equations
- •11.1.1 The Tangential Image
- •11.1.2 The Sagittal Image
- •11.1.3 Astigmatic Calculation
- •11.1.5 Astigmatism for the Three Cases of Zero Spherical Aberration
- •11.1.6 Astigmatism at a Tilted Surface
- •11.2. The Petzval Theorem
- •11.2.1 Relation Between the Petzval Sum and Astigmatism
- •11.2.2 Methods for Reducing the Petzval Sum
- •11.3. Illustration of Astigmatic Error
- •11.4. Distortion
- •11.4.1 Measuring Distortion
- •11.4.2 Distortion Contribution Formulas
- •11.4.3 Distortion When the Image Surface Is Curved
- •11.5. Lateral Color
- •11.5.1 Primary Lateral Color
- •11.6. The Symmetrical Principle
- •11.7. Computation of the Seidel Aberrations
- •11.7.1 Surface Contributions
- •11.7.2 Thin-Lens Contributions
- •11.7.3 Aspheric Surface Corrections
- •11.7.4 A Thin Lens in the Plane of an Image
- •Endnotes
- •12.1.1 Distortion
- •12.1.2 Tangential Field Curvature
- •12.1.3 Coma
- •12.1.4 Spherical Aberration
- •12.2. Simple Landscape Lenses
- •12.2.1 Simple Rear Landscape Lenses
- •12.2.2 A Simple Front Landscape Lens
- •12.3. A Periscopic Lens
- •12.4. Achromatic Landscape Lenses
- •12.4.1 The Chevalier Type
- •12.4.2 The Grubb Type
- •12.5. Achromatic Double Lenses
- •12.5.1 The Rapid Rectilinear
- •12.5.3 Long Telescopic Relay Lenses
- •12.5.4 The Ross “Concentric” Lens
- •Endnotes
- •13.1. The Design of a Dagor Lens
- •13.2. The Design of an Air-Spaced Dialyte Lens
- •13.4. Double-Gauss Lens with Cemented Triplets
- •13.5. Double-Gauss Lens with Air-spaced Negative Doublets
- •Endnotes
- •14.1. The Petzval Portrait Lens
- •14.1.1 The Petzval Design
- •14.1.2 The Dallmeyer Design
- •14.2. The Design of a Telephoto Lens
- •14.3. Lenses to Change Magnification
- •14.3.1 Barlow Lens
- •14.3.2 Bravais Lens
- •14.4. The Protar Lens
- •14.5. Design of a Tessar Lens
- •14.5.1 Choice of Glass
- •14.5.2 Available Degrees of Freedom
- •14.5.3 Chromatic Correction
- •14.5.4 Spherical Correction
- •14.5.5 Correction of Coma and Field
- •14.5.6 Final Steps
- •14.6. The Cooke Triplet Lens
- •14.6.2 The Thin-Lens Predesign of the Bendings
- •14.6.3 Calculation of Real Aberrations
- •14.6.4 Triplet Lens Improvements
- •Endnotes
- •15.1. Comparison of Mirrors and Lenses
- •15.2. Ray Tracing a Mirror System
- •15.3. Single-Mirror Systems
- •15.3.1 A Spherical Mirror
- •15.3.2 A Parabolic Mirror
- •15.3.3 An Elliptical Mirror
- •15.3.4 A Hyperbolic Mirror
- •15.4. Single-Mirror Catadioptric Systems
- •15.4.1 A Flat-Field Ross Corrector
- •15.4.2 An Aplanatic Parabola Corrector
- •15.4.3 The Mangin Mirror
- •15.4.4 The Bouwers–Maksutov System
- •15.4.5 The Gabor Lens
- •15.4.6 The Schmidt Camera
- •15.4.7 Variable Focal-Range Infrared Telescope
- •15.4.8 Broad-Spectrum Afocal Catadioptric Telescope
- •15.4.9 Self-Corrected Unit-Magnification Systems
- •15.5. Two-Mirror Systems
- •15.5.1 Two-Mirror Systems with Aspheric Surfaces
- •15.5.2 A Maksutov Cassegrain System
- •15.5.3 A Schwarzschild Microscope Objective
- •15.5.4 Three-Mirror System
- •15.6. Multiple-Mirror Zoom Systems
- •15.6.2 All-Reflective Zoom Optical Systems
- •15.7. Summary
- •Endnotes
- •16.1. Design of a Military-Type Eyepiece
- •16.1.1 The Objective Lens
- •16.1.2 Eyepiece Layout
- •16.2. Design of an Erfle Eyepiece
- •16.3. Design of a Galilean Viewfinder
- •Endnotes
- •17.1. Finding a Lens Design Solution
- •17.1.1 The Case of as Many Aberrations as There Are Degrees of Freedom
- •17.1.2 The Case of More Aberrations Than Free Variables
- •17.1.3 What Is an Aberration?
- •17.1.4 Solution of the Equations
- •17.2. Optimization Principles
- •17.3. Weights and Balancing Aberrations
- •17.4. Control of Boundary Conditions
- •17.5. Tolerances
- •17.6. Program Limitations
- •17.7. Lens Design Computing Development
- •17.8. Programs and Books Useful for Automatic Lens Design
- •17.8.1 Automatic Lens Design Programs
- •17.8.2 Lens Design Books
- •Endnotes
- •Index
10.6 The Matching Principle |
283 |
10.6 THE MATCHING PRINCIPLE
If we wish to design an aplanatic lens of such a high aperture that a single doublet is impossible, we resort to the use of two achromats in succession. We now have four degrees of freedom. The subdivision of power between the two components and the air space between them is arbitrary, while the two bendings can be used for the correction of spherical aberration and OSC. Any reasonable types of glass can be used, and by achromatizing each component separately we automatically correct both the chromatic aberration and the lateral color.
The design of lenses of this type has been described in detail by Conrady,5 in particular when used as a microscope objective of medium power. Having decided on suitable values for the two arbitrary quantities, we trace a marginal ray through the system from front to back, solving r3 and r6 by the D – d method, and we then add two paraxial rays, one through the front component from left to right using l1 ¼ L1 and u1 ¼ sin U10 , and the other through the rear component from right to left, taking u60 ¼ sin U60 and l60 ¼ L60 as starting data.
If we can now find such a pair of bendings that the two paraxial rays match in the air space between the lenses, the system will be corrected for both spherical aberration and OSC. This is what is meant by the matching principle.
To make the required trial bendings, we have no problem with the front component, but we must adopt standard entry data for the rear component. We can easily adopt a fixed value for L4 by always choosing a suitable air space between the lenses, but any standard value of U4 that we may adopt will never agree exactly with the emerging slope U30 from the front component. Consequently it becomes necessary to match actual aberrations in the air space rather than trying to match lengths and angles.6 So far as lengths are concerned, we have always L4 ¼ L30 – d, and we require that l4 ¼ l30 – d. Subtracting these tells us that we must select bendings such that
LA4 ¼ LA30 |
(10-1) |
To match the slope angles of the paraxial rays in the air space, we have approximately sin U4 ¼ sin U30 , and we require that u4 should also be equal to u30 . Dividing these gives
OSC4 ¼ OSC 30 |
(10-2) |
where the OSC is defined as |
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OSC ¼ ðu= sin UÞ 1 |
(10-3) |
Since this kind of OSC does not contain the usual correcting factor for spherical aberration and exit-pupil position (see Sections 4.3.4 and 9.3), we
284 |
Design of Aplanatic Objectives |
refer to it as uncorrected OSC in the present context. Recall that we are trying to match the ray slope angles in the space between the front and rear components; hence the uncorrected OSC is just a convenient gauge of the relation linking the paraxial and marginal rays. To reiterate, should the matching principle concept of requiring Eqs. (10-1) and (10-2) to be satisfied not be fulfilled, it is certain that the lens system suffers imperfect correction of its aberrations.
As an example to illustrate the matching principle, we will design a 10 microscope objective of numerical aperture 0.25, so that the entering ray slope at the long conjugate end is 0.025. Assuming an object distance of 170 mm, we can trace any desired rays into the front component of the system. It should be noted that, as always, we calculate a microscope objective from the long conjugate to the short, because the long conjugate distance is fixed while the short is not, so that the long-conjugate end becomes the “front” of our system. This conflicts with ordinary microscope parlance, which regards the front of a microscope objective as the short conjugate end; this is a unique exception and we shall ignore it here.
Our first problem is to deal with the two arbitrary degrees of freedom, namely, the subdivision of refracting power between the two components, and the air space between them. For this, it is common to require that the paraxial ray suffers equal deviation at each component, and to place the rear component approximately midway between the front component and its image. This makes the object distance for all rear-element bendings about 20 mm, and we shall adopt that value here.7
As the overall paraxial deviation is 0.25 þ 0.025 ¼ 0.275, we must allow each component to deviate the paraxial ray by 0.1375, which makes the ray slope between the components equal to 0.1125. We shall therefore adopt this value of sin U4 in making all trial bendings of the rear component. For both lenses we use the following common types of glass:
(a)Crown: ne ¼ 1.52520, nF – nC ¼ 0.00893, Ve ¼ 58.81
(b)Flint: ne ¼ 1.62115, nF – nC ¼ 0.01686, Ve ¼ 36.84
with Va – Vb ¼ 21.97. The thin-lens data of the two components (Figure 10.9) are as shown in Table 10.4.
After determining the last radius by the D – d method in every case, the results of several bendings of each component are found to be as shown in Table 10.5. These results are plotted side by side on one graph in Figure 10.10.
0.025
–170
Front
Rear –0.1125 d
–0.25
Figure 10.9 A Lister-type microscope design.
10.6 The Matching Principle |
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Table 10.4 |
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Thin-Lens Data for Lister-type Microscope Shown in Figure 10.9 |
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Object |
Image |
Focal |
Clear |
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distance |
distance |
length |
aperture |
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thicknesses |
(mm) |
(mm) |
(mm) |
(mm) |
ca |
cb |
(mm) |
170 |
37.77 |
30.90 |
8.5 |
0.1649 |
0.0874 |
3.2, 1.0 |
20.0 |
9.00 |
16.36 |
4.5 |
0.3116 |
0.1650 |
2.0, 0.8 |
Table 10.5
Aberrations Versus Bendings for Lister-type Microscope
Front component |
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L1 ¼ l1 ¼ 170.0 |
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sin U1 ¼ u1 ¼ 0.025 |
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c1 |
0 |
0.02 |
0.04 |
0.06 |
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0.08 |
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c3 by D – d |
0.08273 |
0.06254 |
0.04130 |
0.01870 |
þ0.00558 |
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L30 |
33.149 |
34.666 |
35.465 |
35.567 |
35.005 |
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LA03 |
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0.1474 |
0.9529 |
1.3282 |
0.8596 |
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uncorrected OSC30 |
0.01164 |
0.03753 |
0.03727 |
0.01360 |
0.03567 |
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Rear component |
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L4 ¼ 20.00 |
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sin U4 ¼ 0.1125 |
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c4 |
0.05 |
0.10 |
0.15 |
0.20 |
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c6 by D – d |
0.11360 |
0.05405 |
0.01450 |
0.09511 |
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0.19249 |
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L06 ¼ l60 |
7.3552 |
7.3700 |
7.2695 |
7.0888 |
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6.8570 |
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sin U60 ¼ u60 |
0.25862 |
0.24760 |
0.23939 |
0.23259 |
0.22588 |
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l4 |
18.8706 |
20.2829 |
20.7971 |
20.4545 |
19.3870 |
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LA4 |
1.1294 |
0.2829 |
0.7971 |
0.4545 |
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0.6130 |
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uncorrected OSC4 |
0.03222 |
0.03055 |
0.04323 |
0.01363 |
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0.05653 |
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LA′ |
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OSC |
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0.04 |
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OSC |
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Long |
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Middle |
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–1 |
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c1 |
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Figure 10.10 The matching principle.
286 |
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Design of Aplanatic Objectives |
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Table 10.6 |
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Matching Solutions |
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Rectangle |
c1 |
c2 |
c3 |
c4 |
c5 |
c6 |
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A (top) |
0.032 |
0.133 |
0.050 |
0.045 |
0.266 |
0.119 |
B (middle) |
0.067 |
0.098 |
0.010 |
0.070 |
0.242 |
0.091 |
C (bottom) |
0.081 |
0.084 |
0.007 |
0.165 |
0.147 |
0.037 |
D (long) |
0.003 |
0.162 |
0.080 |
0.228 |
0.084 |
0.147 |
It is our aim to select such values of c1 and c4 that LA30 ¼ LA4 and simultaneously OSC30 ¼ OSC4. This is done by searching for rectangles that just fit into the four curves, with spherical aberration and coma points, respectively, each being on the same level. In this case, there are four such rectangles to be found, indicating that the curves represent quadratic expressions. The four solutions are shown in Table 10.6.
For many reasons we shall continue the design using solution C. All the other solutions contain stronger surfaces, and moreover both components of solution C contain almost equiconvex crown elements. This starting setup is as follows:
c |
d |
ne |
0.081
3.21.52520
0.08394
1.01.62115
0.00685
14.9603 (air)
0.165
2.01.52520
0.14654
0.81.62115
0.03730
with l60 ¼ 7.2095, LA60 ¼ 0.01383, u60 ¼ 0.2361, and OSC60 ¼ 0.00297. For the final OSC60 calculation we assumed that the exit pupil is in such a position that (l0 – l0pr) is about 17.0. This puts the exit pupil about 10 mm inside the rear vertex of the objective.
Although this solution is close, we must improve both aberrations by means of a double graph. Changing c1 by 0.001 and maintaining the D – d solutions, and L4 ¼ 20.0, we find that the aberrations become
LA06 ¼ 0:000829; OSC 06 ¼ 0:002404
10.6 The Matching Principle |
287 |
Restoring the original c1 and changing c4 by 0.001 gives |
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LA60 ¼ 0:001306; |
OSC 60 ¼ 0:003279 |
Inspection of the graph suggests that we change the original c1 by 0.001 and c4 by –0.01. These changes give
LA06 ¼ 0:000403; OSC 06 ¼ þ0:000474
Unfortunately the numerical aperture of the system is now 0.2381, whereas it should be 0.25. We therefore scale all radii down by 4%, which gives
LA06 ¼ 0:001114; OSC 06 ¼ 0:000221
Further reference to the double graph suggests that we try Dc1 ¼ 0.0005 and Dc4 ¼ 0.002. This change gives the almost perfect solution drawn to scale in Figure 10.9, namely,
c |
d |
ne |
0.08578
3.2 1.52520
0.08576
1.0 1.62115
0.009152
13.8043 (air)
0.16320
2.0 1.52520
0.16080
0.8 1.62115
0.02602
with l60 ¼ 6.8925, u60 ¼ 0.2500, LA60 ¼ 0.000004, OSC60 ¼ –0.000095, and LZA60 ¼ –0.00289. In practice, of course, we should apply trifling further bendings to both components to render the crown elements exactly equiconvex. These changes are so slight that they have no significant effect on any of the aberrations.
The zonal aberration tolerance is 6l/sin2 Um0 ¼ 0.053, so that the zonal residual of our objective is about half the Rayleigh limit. To improve it, we would have to go to a flint of somewhat higher index, but the present design would be acceptable as it stands.
