Skip to main content
Heliyon logoLink to Heliyon
. 2022 Sep 6;8(9):e10531. doi: 10.1016/j.heliyon.2022.e10531

The determination of secondary ray-aberration coefficients for axis-symmetrical optical systems

Psang Dain Lin 1
PMCID: PMC9474841  PMID: 36119862

Abstract

The ray-aberrations in axis-symmetrical systems are conventionally derived from wavefront functions or characteristic functions using classical approximate partial derivatives. However, the resulting aberrations typically have fifth-order errors, as described by Restrepo et al. (2017) [1]. Accordingly, in the present study, the secondary ray-aberration coefficients for object placed at finite distance are determined using the fifth-order Taylor series expansion of a skew ray. Notably, the derived expressions are exact since they are determined without any approximations. It is found that some of the aberration coefficients are not constants, but are functions of the polar angle of the entrance pupil. It is additionally found that, once the required derivative matrices have been generated, determination of the secondary aberration coefficients is straightforward without iteration, and incurs only a low computational cost.

Keywords: Taylor series expansion, Derivative matrices, Axis-symmetrical system, Ray-aberrations


Taylor series expansion; Derivative matrices; Axis-symmetrical system; Ray-aberrations

1. Introduction

To explore the monochromatic ray-aberrations of an axis-symmetrical system, the object P0=[0h0P0z]T is assumed to be located on the meridional plane at height h0, as shown in Fig. 1. For a ray originating from P0 and passing through the entrance pupil at a point with polar coordinates ρ and ϕ, the intersection point Pn of the ray on the image plane is given by (p. 63 of [2])

Pn=[PnxPnyPnz]=[ΔPnxA2h0+ΔPnyPnz]T, (1)

where A2 is the lateral magnification and ΔPnx and ΔPny are the transverse aberrations of the incidence point in the xn- and yn-directions, respectively, and are given by

ΔPnx=A1ρSϕ+B1ρ3Sϕ+B2(h0ρ2)S(2ϕ)+(B3+B4)(h02ρ)Sϕ+C1ρ5Sϕ+C3(h0ρ4)S(2ϕ)+(C5+C6C2ϕ)(h02ρ3)Sϕ+C9(h03ρ2)S(2ϕ)+C11(h04ρ)Sϕ, (2a)
ΔPny=A1ρCϕ+B1ρ3Cϕ+B2(h0ρ2)(2+C(2ϕ))+(3B3+B4)(h02ρ)Cϕ+B5h03+C1ρ5Cϕ+(C2+C3C2ϕ)(h0ρ4)+(C4+C6C2ϕ)(h02ρ3)Cϕ+[C7+C8C2ϕ](h03ρ2)+C10(h04ρ)Cϕ+C12h05, (2b)

where C and S denote cosine and sine, respectively. (Note that the term C7+C8C(2ϕ) of [2] is replaced by C7+C8C2ϕ in Eq. (2b) in order to satisfy the Buchdahl-Rimmer formulae [3], [4], [5].) The aberrations, ΔPnx and ΔPny, represent the distance by which the ray misses the ideal image point [0A2h0Pnz]T on the image plane, as determined by the paraxial raytracing equation. It is noted that Eqs. (2a) and (2b) contain two first-order terms (referred to as A coefficients), five third-order terms (referred to as B coefficients), and twelve fifth-order terms (referred to as C coefficients).

Figure 1.

Figure 1

Ray originating from an object, passing through an aperture, and then intersecting the image plane.

Smith [2], Zemax [6] and Johanson [7] use different terminologies for describing ray-aberrations. For example, Smith [2] utilizes B1, B2, B3, B4 and B5 to refer to primary spherical aberration, coma, astigmatism, field curvature and distortion, respectively. By contrast, Zemax [6] and Johanson [7] use B1ρmax3, B2h0ρmax2, B3h02ρmax, B4h02ρmax and B5h03, where ρmax is the maximum entrance pupil radius, as the coefficients of spherical aberration, coma, astigmatism, field curvature and distortion, respectively. The aberration coefficients given in [6], [7] are defined as the aberrations at ρ=ρmax for a given h0 since the aberrations at any other value of ρ can be simply determined using an appropriate scaling factor (i.e., (ρ/ρmax)). The present study adopts the notations employed in [6], [7]. Consequently, C1ρmax5 is the secondary spherical aberration coefficient; C2h0ρmax4 and C3h0ρmax4 are the linear coma coefficients; C4h02ρmax3, C5h02ρmax3 and C6h02ρmax3 are the oblique spherical aberration coefficients; C7h03ρmax2, C8h03ρmax2 and C9h03ρmax2 are the elliptical coma coefficients; C10h04ρmax and C11h04ρmax are the Petzval and astigmatism coefficients; and C12h05 is the distortion coefficient.

Aberrations result in significant blurring or distortion of the image. Consequently, effective methods for quantifying their effects during the optical design stage are of paramount importance. The literature contains many approaches for determining the Seidel primary aberration coefficients [8], [9], [10], [11], [12], [13], [14], [15], [16], [17], [18], [19], [20], [21], [22], [23], [24]. One of the most widely used methods in optical software (e.g., Zemax [6]) is that proposed by Buchdahl [8]. However, an alternative approach was recently proposed by Lin and Johnson [23], [24] based on Taylor series expansion of a skew ray. The numerical results of the primary ray-aberrations were shown to be in remarkable agreement with those obtained from Zemax simulations. Consequently, the present study extends this approach to determine the secondary ray-aberration coefficients of an axis-symmetrical system when the object is placed at finite distance. In doing so, a general skew ray Ri is expanded with respect to the source ray variable vector X0 by a Taylor series expansion up to the fifth order. Notably, the obtained equations are exact formulae without approximation. The validity of the proposed method is demonstrated by comparing the computation results with those obtained from Zemax simulations and raytracing, respectively.

2. Variable vectors of source ray

Fig. 2 shows an illustrative axis-symmetrical system with n boundaries when the object is placed at finite position. In accordance with convention, the label i=0 is assigned to the source ray R0=[P00]T originating from the object P0 with height h0, i.e.,

P0=[P0xh0P0z]T. (3)

The unit directional vector of R0 can be defined as

0=[Sα0Cβ0Sβ0Cα0Cβ0]T. (4)

From Eqs. (3) and (4), the independent variable vector of ray R0 is given by

X0=[P0xh0P0zα0β0]T. (5)

Figure 2.

Figure 2

Illustrative axis-symmetrical optical system comprising six elements and eleven boundaries.

In conventional aberration determination, the unit directional vector, 0, is defined in terms of the in-plane coordinates [xaya]T of the entrance pupil (Fig. 3). This representation causes the independent variable vector to be different from that given in Eq. (5), i.e., (Eq. (5) of [24]):

Y0=[P0xh0P0zxa(yah0)]T. (6)

Figure 3.

Figure 3

Entrance pupil with Cartesian coordinates (xa,ya) and polar coordinates (ρ,ϕ).

In exploring the aberrations of object P0=[0h0P0z]T in Fig. 2, a general skew ray Ri should be expanded with respect to the ray originating from point P0,axis=[00P0z]T with unit directional vector 0,axis=[001]T (see Fig. 4). The two independent variables of 0,axis are thus given as α0=β0=xa=ya=0. For convenience, this on-axis ray [P0,axis0,axis]T can be denoted by the following vector:

0axis[00P0z00]T. (7)

It was shown in the Appendix of [24] that the conversion between Eqs. (5) and (6) for the ray defined by Eq. (7) can be achieved by Eq. (8)

f+g+hRih0fxag(yah0)h=f+g+hRih0fα0gβ0h(α0xa)g(β0(yah0))h, (8)

where α0/xa=β0/(yah0)=4.502409965×103. (Note that all lengths and angles given in this study have units of mm and degrees, respectively.)

Figure 4.

Figure 4

Ray with source ray variable vector 0axis.

3. Taylor series expansion of skew ray

In geometrical optics, a general ray Ri is a composite function of Y0 (or X0). The most elegant solution in mathematics for hard problems of this type is the Taylor series expansion since it can provide the polynomial expression of Ri=Ri(Y0) in terms of Y00axis, i.e.,

Ri(Y0)Ri(0axis)+ΔRi=Ri(0axis)+ΔRi/1st+ΔRi/2nd+ΔRi/3rd+ΔRi/4th+ΔRi/5th. (9)

Equation (9) indicates that general ray

Ri(Y0)=[Pix(Y0)Pix(Y0)Piz(Y0)ix(Y0)iy(Y0)iz(Y0)]T

is expanded up to the fifth order. In aberration coefficient determination, the first term in Eq. (9), i.e., Ri(0axis), should be evaluated using the ray defined by 0axis. Furthermore, in aberration exploration, only the two coordinates of the incidence point on the image plane (i.e., Pnx(Y0) and Pny(Y0)) are needed. They can be obtained from the first and second components of Eq. (9) by setting i=n, to have

Pnx(Y0)Pnx(0axis)+ΔPnx/1st+ΔPnx/3rd+ΔPnx/5th, (10a)
Pny(Y0)Pny(0axis)+ΔPny/1st+ΔPny/3rd+ΔPny/5th. (10b)

Note that ΔPnx/2nd=ΔPny/2nd=ΔPnx/4th=ΔPny/4th=0 can be set in Eqs. (10a) and (10b) due to the axis-symmetrical nature of the considered system. The explicit expansions of ΔPnx/1st, ΔPny/1st, ΔPnx/3rd and ΔPny/3rd are given in Eqs. (9a)-(11b) of [24], respectively. Terms Pnx(0axis) and Pny(0axis) in Eqs. (10a) and (10b) are the offsets between the origins of coordinate frame (xyz)n on the image plane and the world coordinate frame (xyz)0, respectively. As such, they have no connection with ray-aberrations, and can hence be ignored. Terms ΔPnx/1st and ΔPny/1st determine the defocus aberration coefficient A1 and transverse magnification A2, respectively, while ΔPnx/3rd and ΔPny/3rd can be used to explore the B aberration coefficients [24]. The complete expression of ΔPnx/5th in Eq. (10a), (10b)(a) has the form

ΔPnx/5th=1120[5Pnxh05h05+55Pnxh04xah04xa+55Pnxh04(yah0)h04(yah0)+105Pnxh03xa2h03xa2+205Pnxh03xa(yah0)h03xa(yah0)+105Pnxh03(yah0)2h03(yah0)2+105Pnxh02xa3h02xa3+305Pnxh02xa2(yah0)h02xa2(yah0)+305Pnxh02xa(yah0)2h02xa(yah0)2+105Pnxh02(yah0)3h02(yah0)3+55Pnxh0xa4h0xa4+205Pnxh0xa3(yah0)h0xa3(yah0)+305Pnxh0xa2(yah0)2h0xa2(yah0)2+205Pnxh0xa(yah0)3h0xa(yah0)3+55Pnxh0(yah0)4h0(yah0)4+5Pnxxa5xa5+55Pnxxa4(yah0)xa4(yah0)+105Pnxxa3(yah0)2xa3(yah0)2+105Pnxxa2(yah0)3xa2(yah0)3+55Pnxxa(yah0)4xa(yah0)4+5Pnx(yah0)5(yah0)5]. (11)

Meanwhile, the complete expression of ΔPny/5th in Eq. (10b) can be obtained from Eq. (11) by simply substituting Pny for Pnx.

Due to the axis-symmetrical nature of the considered system, various terms in Eq. (11) disappear (as confirmed by our numerical results), and hence the expressions of ΔPnx/5th and ΔPny/5th become

ΔPnx/5th=1120(5Pnxxa5xa5+105Pnxxa3(yah0)2xa3(yah0)2+55Pnxxa(yah0)4xa(yah0)4+205Pnxh0xa3(yah0)h0xa3(yah0)+205Pnxh0xa(yah0)3h0xa(yah0)3+105Pnxh02xa3h02xa3+305Pnxh02xa(yah0)2h02xa(yah0)2+205Pnxh03xa(yah0)h03xa(yah0)+55Pnxh04xah04xa), (12a)
ΔPny/5th=1120(55Pnyxa4(yah0)xa4(yah0)+105Pnyxa2(yah0)3xa2(yah0)3+5Pny(yah0)5(yah0)5+55Pnyh0xa4h0xa4+305Pnyh0xa2(yah0)2h0xa2(yah0)2+55Pnyh0(yah0)4h0(yah0)4+305Pnyh02xa2(yah0)h02xa2(yah0)+105Pnyh02(yah0)3h02(yah0)3+105Pnyh03xa2h03xa2+105Pnyh03(yah0)2h03(yah0)2+55Pnyh04(yah0)h04(yah0)+5Pnyh05h05). (12b)

As shown, Eqs. (12a) and (12b) are both expressed with respect to the object height h0 and in-plane Cartesian coordinates (xa,ya) of the entrance pupil. However, aberration equations are usually expressed in terms of the polar coordinates of the entrance pupil, i.e., (ρ,ϕ) (Fig. 3). Hence, it is necessary to replace (xa,ya) in Eqs. (12a) and (12b) with (ρSϕ,ρCϕ). The following equations are thus obtained:

ΔPnx/5th=fx/0ρ5Sϕ+fx/1(h0ρ4)S2ϕ+fx/2(h02ρ3)Sϕ+fx/3(h03ρ2)S(2ϕ)+fx/4(h04ρ)Sϕ, (13a)
ΔPny/5th=fy/0ρ5Cϕ+fy/1(h0ρ4)+fy/2(h02ρ3)Cϕ+fy/3(h03ρ2)+fy/4(h04ρ)Cϕ+fy/5h05. (13b)

The leading coefficients of Eqs. (13a) and (13b) are given respectively by

fx/0=1120(5Pnxxa5S4ϕ+55Pnxxa(yah0)4C4ϕ+105Pnxxa3(yah0)2S2ϕC2ϕ), (14a)
fx/1=112(5Pnxxa(yah0)45Pnxh0xa(yah0)3)C2ϕ112(5Pnxxa3(yah0)25Pnxh0xa3(yah0))S2ϕ, (14b)
fx/2=14(5Pnxxa(yah0)425Pnxh0xa(yah0)3+5Pnxh02xa(yah0)2)C2ϕ+112(5Pnxxa3(yah0)225Pnxh0xa3(yah0)+5Pnxh02xa3)S2ϕ, (14c)
fx/3=112(5Pnxxa(yah0)4+35Pnxh0xa(yah0)335Pnxh02xa(yah0)2+5Pnxh03xa(yah0)), (14d)
fx/4=124(5Pnxxa(yah0)445Pnxh0xa(yah0)3+65Pnxh02xa(yah0)245Pnxh03xa(yah0)+5Pnxh04xa), (14e)
fy/0=1120(5Pny(yah0)5C4ϕ+55Pnyxa4(yah0)S4ϕ+105Pnyxa2(yah0)3S2ϕC2ϕ), (15a)
fy/1=124(5Pnyh0xa45Pnyxa4(yah0))S4ϕ+14(5Pnyh0xa2(yah0)25Pnyxa2(yah0)3)S2ϕC2ϕ+124(5Pnyh0(yah0)45Pny(yah0)5)C4ϕ, (15b)
fy/2=14(5Pnyxa2(yah0)325Pnyh0xa2(yah0)2+5Pnyh02xa2(yah0))S2ϕ+112(5Pny(yah0)525Pnyh0(yah0)4+5Pnyh02(yah0)3)C2ϕ, (15c)
fy/3=112(5Pnyh03xa25Pnyxa2(yah0)3+35Pnyh0xa2(yah0)235Pnyh02xa2(yah0))S2ϕ112(5Pny(yah0)55Pnyh03(yah0)2+35Pnyh02(yah0)335Pnyh0(yah0)4)C2ϕ, (15d)
fy/4=124(5Pny(yah0)545Pnyh0(yah0)4+65Pnyh02(yah0)345Pnyh03(yah0)2+5Pnyh04(yah0)), (15e)
fy/5=1120(5Pny(yah0)5+55Pnyh0(yah0)4105Pnyh02(yah0)3+105Pnyh03(yah0)255Pnyh04(yah0)+5Pnyh05). (15f)

Equations (10a) and (10b) are derived independently from other aberration theory. However, Eqs. (2a) and (2b) are obtained from the wavefront aberration function W(h0,ρ,ϕ) by using the following approximate partial derivatives [1]:

ΔPnxRreferenceξWxa, (16a)
ΔPnyRreferenceξWya, (16b)

where Rreference and ξ are the radius and refractive index of the reference sphere, respectively. As discussed by Restrepo et al. [1], Eqs. (16a) and (16b) inevitably induce errors as a result of their approximate nature. Furthermore, Sasián pointed out that these errors are of the fifth order (p. 102 of [17]). Figure 5, Figure 6 compare the values of Pnx and Pny obtained from Eqs. (1), (10a) and (10b) for the system shown in Fig. 2 (its parameters are given in Table 1) with those obtained from raytracing. The values of the A, B and C aberration coefficients computed by Zemax [6] for the considered system are listed in Table 2 of the present study for the case where the object is placed at P0=[017200] and the maximum entrance pupil radius is ρmax=21. The computed curves in Figure 5, Figure 6 show the interception coordinates on the Gaussian image plane of rays originating from P0 and striking the entire rim of the entrance pupil (i.e., 0ϕ<360) with ρmax=21. Curves Pnx(Y0) and Pny(Y0) are obtained from raytracing, and are thus marred by higher-order aberrations. By contrast, the computed curves from Eq. (1), Eqs. (10a) and (10b) consist only of the zero- to fifth-order series. It is seen in Fig. 5 that the curves obtained from Eq. (1) and Eq. (10a) are almost overlaid for 0ϕ<360. Similarly, in Fig. 6, the curves obtained from Eq. (1) and Eq. (10b) are indistinguishable except for the region near ϕ=180. Consequently, it is reasonable to infer that the secondary ray-aberration coefficients obtained using the proposed method in the present study (see the following section) will not deviate too much with those obtained from Zemax.

Figure 5.

Figure 5

Comparison of results obtained from Eqs. (1) and (10a) for Pnx with those obtained from raytracing.

Figure 6.

Figure 6

Comparison of results obtained from Eqs. (1) and (10b) for Pny with those obtained from raytracing.

Table 1.

Specification of illustrative rotationally-symmetric optical system shown in Fig. 2.

Surface Radius Separation Refractive index
0 (object) 200.00000 1.00000
1 38.22190 15.84960 1.65000
2 -56.08570 5.96900 1.71736
3 -590.68200 3.02260 1.00000
4 (aperture) 14.02080 1.00000
5 -41.79570 2.514600 1.52583
6 29.34460 7.924800 1.00000
7 63.56350 6.09600 1.65000
8 -56.86550 92.088474 1.00000
9 (image plane) Image 1 Image 1

Table 2.

Values of aberration coefficients obtained from Zemax simulations.

A1 = 0.000000 A2 = −0.660413 B1ρmax3=1.533486
B2h0ρmax2=0.112776 B3h02ρmax=8.16154×103 B4h02ρmax=0.033624
C1ρmax5=0.075594 C2h0ρmax4=0.090476 C3h0ρmax4=0.067381
C4h02ρmax3=0.090356 C5h02ρmax3=0.033730 C6h02ρmax3=0.067592
C7h03ρmax2=0.010459 C8h03ρmax2=0.032328 C9h03ρmax2=0.009668
C10h04ρmax=0.001088 C11h04ρmax=0.001406 C12h05=0.0006322

4. Results of secondary ray-aberration coefficients

In this section, the values of the secondary ray-aberration coefficients are determined for the axis-symmetrical system shown in Fig. 2 (with the object positioned at P0z=200, the image plane coinciding with the Gaussian image plane, and the maximum radius of the entrance pupil being ρmax=21). The symbols in Eqs. (2a) and (2b) are still used under the assumption that they are functions of ϕ. One has the following equations from Eqs. (2a) and (2b) by taking only the terms with C coefficients:

ΔPnx/5th=C1ρ5Sϕ+C3(h0ρ4)S(2ϕ)+(C5+C6C2ϕ)(h02ρ3)Sϕ+C9(h03ρ2)S(2ϕ)+C11(h04ρ)Sϕ, (17a)
ΔPny/5th=C1ρ5Cϕ+(C2+C3C2ϕ)(h0ρ4)+(C4+C6C2ϕ)(h02ρ3)Cϕ+[C7+C8C2ϕ](h03ρ2)+C10(h04ρ)Cϕ+C12h05. (17b)

It is noted that coefficients C3 and C6 are used in Eq. (17b) to take account of possible differences in the expressions and possible errors arising from the approximation of Eqs. (16b). One thus has the following equations by comparing Eqs. (13a) and (13b) with Eqs. (17a) and (17b), respectively:

C1=fx/0, (18a)
C3=fx/1, (18b)
C5+C6C2ϕ=fx/2, (18c)
C9=fx/3, (18d)
C11=fx/4, (18e)
C1=fy/0, (19a)
C2+C3C2ϕ=fy/1, (19b)
C4+C6C2ϕ=fy/2, (19c)
C7+C8C2ϕ=fy/3, (19d)
C10=fy/4, (19e)
C12=fy/5. (19f)

Since Eqs. (16a) and (16b) are not exact equations and possess fifth-order errors [1], it is possible that the values obtained in this study are different from those of Zemax. Therefore, the following percentage difference metric is introduced to compare the results obtained using the proposed method with those obtained from Zemax simulations:

Ck%=100|(Ck/thisCk/zemax)wk/zemax|, (20)

where Ck/this and Ck/zemax of Eq. (20) are the kth (k=1-12) aberration coefficient values obtained from the proposed method and Zemax simulations, respectively.

(1) C1 coefficient: The spherical aberration is the only fifth-order term which does not depend on h0. From Eqs. (18a) and (14a), C1 can be expressed as

C1=C1zero+C1twoS2ϕ+C1fourS4ϕ, (21a)

where

C1zero=1245Pnxxa(yah0)4, (21b)
C1two=112(5Pnxxa3(yah0)25Pnxxa(yah0)4), (21c)
C1four=1120(5Pnxxa5+55Pnxxa(yah0)4105Pnxxa3(yah0)2). (21d)

Meanwhile, from Eqs. (19a) and (15a), C1 can also be expressed as

C1=C1zero+C1twoC2ϕ+C14C4ϕ, (21e)

where

C1zero=1245Pnyxa4(yah0), (21f)
C1two=112(5Pnyxa2(yah0)35Pnyxa4(yah0)), (21g)
C1four=1120(5Pny(yah0)5+55Pnyxa4(yah0)105Pnyxa2(yah0)3). (21h)

If C1 is determined from Eq. (21a) by setting ϕ=90, or from Eq. (21e) by setting ϕ=0, the following value is obtained:

C1=C1zero+C1two+C1four=218.65267×1010. (21i)

The value of the secondary spherical aberration coefficient can be obtained from Eq. (21i) as

C1/this=C1ρmax5=0.089300. (21j)

This value differs by C1%=18.1% from the value obtained by Zemax simulations (C1/zemax=0.075594).

(2) C2 and C3 coefficients: Equations (18b) and (14b) show that C3 can be expressed as

C3=C3zero+C3twoS2ϕ, (22a)

where

C3zero=112(5Pnxxa(yah0)45Pnxh0xa(yah0)3), (22b)
C3two=112(5Pnxxa(yah0)45Pnxh0xa(yah0)3)112(5Pnxxa3(yah0)25Pnxh0xa3(yah0)). (22c)

Furthermore, from Eqs. (19b) and (15b), C3 can be expressed as the following function of ϕ:

C3=C3twoC2ϕ+C3fourC4ϕ. (22d)

From Eqs. (15b), (19b) and (22d), the expressions for C2, C3two and C3four are obtained as

C2=124(5Pnyh0xa45Pnyxa4(yah0)), (22e)
C3two=112(5Pnyh0xa45Pnyxa4(yah0))+14(5Pnyh0xa2(yah0)25Pnyxa2(yah0)3), (22f)
C3four=124(5Pnyh0xa45Pnyxa4(yah0))14(5Pnyh0xa2(yah0)25Pnyxa2(yah0)3)+124(5Pnyh0(yah0)45Pny(yah0)5). (22g)

The values of the linear coma aberration coefficient are obtained from Eq. (22e) as C2/this=C2ρmax4h0=0.018219. The other two linear coma aberration coefficients are found from Eq. (22a) with ϕ=90 and Eq. (22d) with ϕ=0 to be C3/this=(C3zero+C3two)ρmax4h0=0.062674 and C3/this=(C3two+C3four)ρmax4h0=0.108368, respectively. These values deviate by C2%=79.9%, C3%=7.0% and C3%=60.8% from the corresponding Zemax results (i.e., C2/zemax=0.090476 and C3/zemax=C3/zemax=0.067381).

(3) C4, C5 and C6 coefficients: From Eqs. (18c) and (14c), one has the following analytical expressions for C5 and C6:

C5=112(5Pnxxa3(yah0)225Pnxh0xa3(yah0)+5Pnxh02xa3), (23a)
C6=14(5Pnxxa(yah0)425Pnxh0xa(yah0)3+5Pnxh02xa(yah0)2)112(5Pnxxa3(yah0)225Pnxh0xa3(yah0)+5Pnxh02xa3). (23b)

Moreover, the following expressions for C4 and C6 are obtained from Eqs. (19c) and (15c):

C4=14(5Pnyxa2(yah0)325Pnyh0xa2(yah0)2+5Pnyh02xa2(yah0)), (23c)
C6=14(5Pnyxa2(yah0)325Pnyh0xa2(yah0)2+5Pnyh02xa2(yah0))+112(5Pny(yah0)525Pnyh0(yah0)4+5Pnyh02(yah0)3). (23d)

From Eqs. (23c), (23a), (23b) and (23d), coefficients C4, C5, C6 and C6 have values of C4=313.038676×1010, C5=128.793685×1010, C6=188.76106×1010 and C6=194.629533×1010, respectively. Consequently, the oblique spherical aberration coefficients have values of C4/this=C4h02ρmax3=0.083783, C5/this=C5h02ρmax3=0.034471, C6/this=C6h02ρmax3=0.050521 and C6/this=C6h02ρmax3=0.052091. These values deviate from the corresponding Zemax results (i.e., C4/zemax=0.090356, C5/zemax=0.033730 and C6/zemax=0.067592) by C4%=7.3%, C5%=2.2%, C6%=25.3% and C6%=22.9%, respectively.

(4) C7, C8 and C9 coefficients: The expressions of C7 and C8 are obtained from Eqs. (19d) and (15d), respectively, as

C7=112(5Pnyh03xa25Pnyxa2(yah0)3+35Pnyh0xa2(yah0)235Pnyh02xa2(yah0)), (24a)
C8=112(5Pnyh03xa25Pnyxa2(yah0)3+35Pnyh0xa2(yah0)235Pnyh02xa2(yah0))112(5Pny(yah0)55Pnyh03(yah0)2+35Pnyh02(yah0)335Pnyh0(yah0)4). (24b)

From Eqs. (24a), (24b) and (18d), coefficients C7, C8 and C9 have values of C7=36.93595×1010, C8=144.98793×1010 and C9=36.48465×1010, respectively. Moreover, the elliptical coma coefficients have values of C7/this=C7h03ρmax2=0.008003, C8/this=C8h03ρmax2=0.031413 and C9/this=C9h03ρmax2=0.007906, and thus deviate by C7%=23.5%, C8%=2.8% and C9%=18.2% from the corresponding Zemax results (i.e., C7/zemax=0.010459, C8/zemax=0.032328 and C9/zemax=0.009668).

(5) C10 and C11 coefficients: From Eqs. (19e) and (18e), C10 and C11 can be obtained as

C10=12.00188×1010, (25a)
C11=10.04826×1010. (25b)

From Eqs. (25a) and (25b), the Petzval coefficient and astigmatism coefficients have values of C10/this=C10h04ρmax=0.002105 and C11/this=C11h04ρmax=0.001762, respectively. These values deviate by C10%=93.5% and C11%=25.4% from the corresponding Zemax results (i.e., C10/zemax=0.001088 and C11/zemax=0.001406).

(6) C12 coefficient: From Eq. (19f), coefficient C12 is obtained as

C12=4.55416×1010. (26)

The fifth-order distortion coefficients determined from Eq. (26) and Zemax simulations, respectively, are C12/this=C12h05=6.46626×104 and C12/zemax=6.3220×104. In other words, the two values differ by just C12%=2.3%. The values of C aberration coefficients are summarized in Table 3.

Table 3.

Values of C aberration coefficients obtained from the proposed method.

C1ρmax5=0.089300 C2ρmax4h0=0.018219 (C3zero+C3two)ρmax4h0=0.062674
(C3two+C3four)ρmax4h0=0.108368 C4h02ρmax3=0.083783 C5h02ρmax3=0.034471
C6h02ρmax3=0.050521 C6h02ρmax3=0.052091 C7h03ρmax2=0.008003
C8h03ρmax2=0.031413 C9h03ρmax2=0.007906 C10h04ρmax=0.002105
C11h04ρmax=0.001762 C12h05=6.46626×104 Image 2

5. Conclusions

The aberrations of an optical system can be described in terms of the wavefront aberration and ray-aberration and are commonly related using the approximations given in Eqs. (16a) and (16b). However, the obtained expressions for the ray-aberrations, given in Eqs. (2a) and (2b), have errors of a fifth order. Restrepo et al. [1] found that Eqs. (2a) and (2b) thus yield large errors for systems with large numerical apertures. Accordingly, in previous studies [23], [24], the present group proposed a new method for determining the aberration coefficients of the primary ray based on the Taylor series expansion of a skew ray. In the present study, this method has been extended to determine the secondary ray-aberration coefficients when the object is placed at finite position. The Taylor series expansion decomposes the aberrations into different orders without approximation, and hence the resulting expressions are exact. It has been shown that some of the secondary ray-aberration coefficients are functions of the polar angle of the entrance pupil. It is further noted that, once the derivative matrices have been generated, determination of the aberration coefficients is straightforward without iteration, and hence incurs only a low computational cost.

Declarations

Author contribution statement

Psang Dain Lin: Conceived and designed the analysis; Analyzed and interpreted the data; Contributed analysis tools or data; Wrote the paper.

Funding statement

Professor Psang Dain Lin was supported by Ministry of Science and Technology, Taiwan (MOST) (111-2221-E-006-138-).

Data availability statement

Data included in article/supp. material/referenced in article.

Declaration of interests statement

The authors declare no conflict of interest.

Additional information

No additional information is available for this paper.

Acknowledgements

The support, motivation and encouragement offered by my colleague, Professor R. Barry Johnson (Alabama Agricultural & Mechanical University) throughout the study of ray-aberrations is greatly appreciated.

References

  • 1.Restrepo J., Stoerck P.J., Ihrke I. Ray and wave aberration revisited: a Huygens-like construction yields exact relations. J. Opt. Soc. Am. 2017;34:1856–1864. doi: 10.1364/JOSAA.33.000160. [DOI] [PubMed] [Google Scholar]
  • 2.Smith W.J. 3rd ed. Edmund Industrial Optics; Barrington, N.J.: 2001. Modern Optical Engineering. [Google Scholar]
  • 3.Rosete-Aguilar M., Rayces J.L. Renormalization of the Buchdahl-Rimmer coefficients of the reduced geometric aberration functions to RMS spot size. J. Mod. Opt. 1996;43:685–692. [Google Scholar]
  • 4.Rosete-Aguilar M., Rayces J.L. Renormalization of the Buchdahl-Rimmer third- and fifth-order geometric aberration coefficients to RMS wave aberration function expressions. J. Mod. Opt. 1995;19:2435–2445. [Google Scholar]
  • 5.Rosete-Aguilar M., Rayces J.L. Renormalization of Buchdahl-Rimmer aberration coefficients to RMS expressions. Proc. SPIE. 1996;2730 [Google Scholar]
  • 6.Zemax optical design program user's guide, 2013.
  • 7.Kingslake R., Johnson R.B. second edition. Academic; 2010. Lens Design Fundamentals. [Google Scholar]
  • 8.Buchdahl H.A. Dover Publications; New York: 1968. Optical Aberration Coefficients. [Google Scholar]
  • 9.Welford W.T. Hilger; Bristol, UK: 1986. Aberrations of Optical Systems. [Google Scholar]
  • 10.Hopkins G.W. Proximate ray tracing and optical aberration coefficients. J. Opt. Soc. Am. 1976;66:405–410. [Google Scholar]
  • 11.Welford W.T. A new total aberration formula. J. Mod. Opt. 1972;19:719–727. [Google Scholar]
  • 12.Chen B., Herkommer A.M. High order surface aberrations contributions from phase space analysis of differential rays. Opt. Express. 2016;24:5934–5945. doi: 10.1364/OE.24.005934. [DOI] [PubMed] [Google Scholar]
  • 13.Oleszko M., Hambach R., Gros H. Decomposition of the total wave aberration in generalized optical systems. J. Opt. Soc. Am. 2017;34:1856–1864. doi: 10.1364/JOSAA.34.001856. [DOI] [PubMed] [Google Scholar]
  • 14.Bociort F., Kross J. Seidel aberration coefficients for radial gradient-index lenses. J. Opt. Soc. Am. 1994;11:2647–2656. [Google Scholar]
  • 15.Claus D., Watson J., Rodenburg J. Analysis and interpretation of the Seidel aberration coefficients in digital holography. Appl. Opt. 2011;50:H220–H229. doi: 10.1364/AO.50.00H220. [DOI] [PubMed] [Google Scholar]
  • 16.Chang R.S., Sheu J.Y., Lin C.H. Analysis of Seidel aberration by use of the discrete wavelet transform. Appl. Opt. 2002;41:2408–2413. doi: 10.1364/ao.41.002408. [DOI] [PubMed] [Google Scholar]
  • 17.Sasián J. Cambridge University; 2013. Introduction to Aberrations in Optical Imaging Systems. [Google Scholar]
  • 18.Johnson R.B. Polynomial ray aberrations computed in various lens design programs. Appl. Opt. 1973;12:2079–2082. doi: 10.1364/AO.12.002079. [DOI] [PubMed] [Google Scholar]
  • 19.Lin P.D. Determination of secondary wavefront aberrations in axis-symmetrical optical systems. Appl. Comput. Math. May 2022;11(3):60–68. [Google Scholar]
  • 20.Lin P.D. It is a sufficient condition only, not a necessary and sufficient condition, for decomposing wavefront aberrations. J. Eur. Opt. Soc., Rapid Publ. July 2022;18(3):1–4. [Google Scholar]
  • 21.Johnson R.B. Image defects useful in teaching students. Proc. SPIE. 1987;766:10–17. [Google Scholar]
  • 22.Johnson R.B. Balancing the astigmatic fields when all other aberrations are absent. Appl. Opt. 1993;32:3494–3496. doi: 10.1364/AO.32.003494. [DOI] [PubMed] [Google Scholar]
  • 23.Lin P.D., Johnson R.B. Seidel aberration coefficients: an alternative computation method. Opt. Express. 2019;27(14):19712–19725. doi: 10.1364/OE.27.019712. [DOI] [PubMed] [Google Scholar]
  • 24.Lin P.D. Seidel primary ray aberration coefficients for objects placed at finite and infinite distances. Opt. Express. 2020;28(9):19740–19754. doi: 10.1364/OE.390346. [DOI] [PubMed] [Google Scholar]

Associated Data

This section collects any data citations, data availability statements, or supplementary materials included in this article.

Data Availability Statement

Data included in article/supp. material/referenced in article.


Articles from Heliyon are provided here courtesy of Elsevier

RESOURCES