Zoom lens system having a camera shake compensating function

Abstract

A zoom lens system includes from the object side a first lens unit of a positive refractive power, a second lens unit of a positive refractive power, an aperture stop and a third lens unit of a negative refractive power. The second lens unit includes a front lens unit of a negative refractive power and a rear lens unit of a positive refractive power. In zooming from the shorter focal length side to the longer focal length side, the distance between the first and second lens units increases and the distance between the second and third lens units varies. Camera shake is compensated for by parallel decentering the entire second lens unit.

Description

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to a zoom lens system having a camera shake compensating function, and more specifically, to a zoom lens system having a camera shake compensating function suitable for use in a lens shutter camera, capable of preventing image blur due to camera shake (i.e. shake of the camera caused when the user holds the camera to perform photographing).

2. Description of the Prior Art

Conventionally, the failure in photographing was mostly attributed to camera shake and being out of focus. In recent years; however, most cameras employ the automatic focusing mechanism and with the improvement of focusing accuracy of the automatic focusing mechanism, the problem of the failure in photographing due to being out of focus has been practically solved. On the other hand, the lens system normally incorporated in the camera has shifted from a fixed focal length lens system to a zoom lens system, and with the shift, the magnification and the longest focal length have been increased. Consequently, camera shake very frequently occurs. As a result, presently, it is no exaggeration to say that a major cause of failure in photographing is caused by camera shake. For this reason, a camera shake compensating function can be indispensable for the zoom lens system.

As zoom lens systems having a camera shake compensating function, zoom lens systems have been proposed in which camera shake is compensated for by decentering a part of the lens (Japanese Laid-open Patent Applications Nos. H1-116619, H2-103014, H2-93620, H4-362909, H4-212916 and H6-95039).

In a zoom lens system having a camera shake compensating function, not only the optical performance is excellent in a standard condition (hereinafter, sometimes referred to as “predecentering condition”) but also the generation of aberrations (hereinafter, referred to as “decentering aberrations”) caused by the decentering of the lens is curbed to maintain the optical performance in a compensated condition (hereinafter, sometimes referred to as “post-decentering condition). In the above-mentioned prior arts, however, since the degradation of optical performance due to the decentering is great, sufficient optical performance is not obtained in the entire zoom range. Furthermore, the increase in magnification and the reduction in size are not sufficiently achieved.

SUMMARY OF THE INVENTION

An object of the present invention is to provide a high-magnification, compact zoom lens system having a camera shake compensating function, capable of compensating camera shake while maintaining high optical performance in the entire zoom range.

BRIEF DESCRIPTION OF THE DRAWINGS

This and other objects and features of this invention will become clear from the following description, taken in conjunction with the preferred embodiments with reference to the accompanied drawings in which:

FIG. 1 shows the lens arrangement of a first embodiment of the present invention;

FIG. 2 shows the lens arrangement of a second embodiment of the present invention;

FIGS. 3A to 3 F show longitudinal aberrations of the first embodiment before centering;

FIGS. 4A to 4 F show longitudinal aberrations of the second embodiment before decentering;

FIGS. 5A to 3 B show meridional lateral aberrations of the first embodiment at the shortest focal length condition before decentering;

FIGS. 5C to 5 E show meridional lateral aberrations of the first embodiment the shortest focal length condition after decentering;

FIGS. 6A to 6 B show sagittal lateral aberrations of the first embodiment at the shortest focal length condition before decentering;

FIGS. 6C to 6 E show sagittal lateral aberrations of the first embodiment at the shortest focal length condition after decentering;

FIGS. 7A to 7 B show meridional lateral aberrations of the first embodiment at the longest focal length condition before decentering;

FIGS. 7C to 7 E show meridional lateral aberrations of the first embodiment at the longest focal length condition after decentering;

FIGS. 8A to 8 B show sagittal lateral aberrations of the first embodiment at the longest focal length condition before decentering;

FIGS. 8C to 8 E show sagittal lateral aberrations of the first embodiment at the longest focal length condition after decentering;

FIGS. 9A to 9 B show meridional lateral aberrations of the second embodiment at the shortest focal length condition before decentering;

FIGS. 9C to 9 E show meridional lateral aberrations of the second embodiment at the shortest focal length condition after decentering;

FIGS. 10A to 10 B show sagittal lateral aberrations of the second embodiment at the shortest focal length condition before decentering;

FIGS. 10C to 10 E show sagittal lateral aberrations of the second embodiment at the shortest focal length condition after decentering;

FIGS. 11A to 11 B show meridional lateral aberrations of the second embodiment at the longest focal length condition before decentering;

FIGS. 11C to 11 E show meridional lateral aberrations of the second embodiment at the longest focal length condition after decentering;

FIGS. 12A to 12 B show sagittal lateral aberrations of the second embodiment at the longest focal length condition before decentering;

FIGS. 12C to 12 E show sagittal lateral aberrations of the second embodiment at the longest focal length condition after decentering;

FIGS. 13A to 13 D are views of assistance in explaining the factors of image degradation of the camera shake compensating optical system;

FIG. 14 is view of assistance in explaining a relationship between optical system and the coordinates;

FIGS. 15A to 15 B are views of assistance in explaining the difference in light beam passing position due to decentering;

FIG. 16 is a view of assistance in explaining rotational conversion of the object surface;

FIG. 17 is a view of assistance in explaining aberration coefficients of reversal and non-reversal optical systems;

FIGS. 18A to 18 B show are views of assistance in explaining rotational conversion; and

FIG. 19 is a view of assistance in explaining conversion to the image surface.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

A zoom lens system having a camera shake compensating function according to a first implementation of the present invention comprises from the object side a first lens unit of a positive refractive power, a second lens unit of a positive refractive power, an aperture stop and a third lens unit of a negative refractive power. The second lens unit includes from the object side a front lens unit of a negative refractive power and a rear lens unit of a positive refractive power. Zooming is performed by varying the distance between the first and second lens units and the distance between the second and third lens units so that the distance between the first and second lens units increases in zooming from the shorter focal length side to the longer focal length side. Camera shake is compensated for by parallelingly decentering the entire second lens unit.

A zoom lens system having a camera shake compensating function according to a second implementation of the present invention comprises from the object side a first lens unit of a positive refractive power, a second lens unit of a positive refractive power, an aperture stop and a third lens unit of a negative refractive power. The second lens unit includes from the object side a front lens unit of a negative refractive power and a rear lens unit of a positive refractive power. Zooming is performed by varying the distance between the first and second lens units and the distance between the second and third lens units so that the distance between the first and second lens units increases in zooming from the shorter focal length side to the longer focal length side. Camera shake is compensated for by parallelingly decentering the entire second lens unit. Further, the following conditions (1) and (2) are fulfilled: $$ 0 < φ I φ W < 0.57 ( 1 ) 0.03 < φ DF C DR < 0.5 ( 2 )

where φ I is a refractive power of the first lens unit, φ W is a refractive power of the entire lens system at the shortest focal length condition, φ DF is a refractive power of the front lens unit (i.e. the negative lens unit on the object side) of the second lens unit, and C DR is a curvature of the most image side surface of the second lens unit.

The parallel decentering is to move a part of the optical system in a direction vertical (or substantially vertical) to the optical axis. In the present invention, as the optical system (hereinafter, referred to as “compensation lens unit”) parallelingly decentered for camera shake compensation, the entire second lens unit (i.e. all the lens elements of the second lens unit) which is one of the zooming lens units is used. Since aberrations in the zooming lens units are typically corrected within the lens units, with this arrangement, not only aberrations in the standard condition but also the decentering aberrations are corrected more excellently than in the prior art (e.g. Japanese Laid-open Patent Applications Nos. H2-103014, H2-93620, H4-362909 and H6-95039). On the contrary, when camera shake is compensated for by decentering a part of the lens units constituting the zooming lens units, it is necessary to correct aberrations by the part of the lens units and further by the entire zoom lens units, so that the number of lens elements increases to increase the total length of the lens system.

Since the second lens unit serving as a compensation lens unit is of a negative, positive configuration and an aperture stop is arranged therebehind, distortion is made negative (aberration coefficient V is positive) by the second lens unit. Since the off-axial image point movement error caused thereby is positive, the negative off-axial image point error invariably generated by rotational camera shake is canceled more effectively than in the prior art (e.g. Japanese Laid-open Patent Application No. H1-116619).

In a zoom lens system which includes only a positive compensation lens unit and a negative lens unit and in which the distance between the lens units increases in zooming toward the longer focal length side, the magnitude of lateral chromatic aberration largely differs between on the shorter focal length side and on the longer focal length side. Further, since axial lateral chromatic aberration caused by the decentering is added thereto in camera shake compensation, the total of the lateral chromatic aberration is impermissible. In the present invention, to excellently correct the lateral chromatic aberration, a positive lens unit (first lens unit) in which the distance from the compensation lens unit increases in zooming toward the longer focal length side is arranged in front of the compensation lens unit.

When the first lens unit is negative (when the lower limit of the condition (1) is exceeded), large negative distortion is generated in the first lens unit, so that the off-axial image a point movement error increases toward the positive side. When the refractive power of the first lens unit is too high toward the positive side (when the upper limit of the condition (1) is exceeded), a large positive distortion is generated in the first lens unit, so that the off-axial image point movement error increases toward the negative side. Therefore, by fulfilling the condition (1), distortion is corrected excellently and the off-axial image point movement error is restrained to be small compared to the prior art (e.g. Japanese Laid-open Patent Applications Nos. H1-116619 and H4-212916).

It is preferable that the most image side surface (i.e. the surface closest to the aperture stop) of the second lens unit serving as a compensation lens unit is convex to the image side. The negative front lens unit of the second lens unit generates negative distortion and large positive spherical aberration (aberration coefficient I is negative) and causes the generation of axial coma in camera shake compensation on the longer focal length side. If the most aperture stop side surface of the compensation lens unit is (comparatively strongly) convex to the image side, since the surface is close to the aperture stop, the surface does not generate distortion but generates negative spherical aberration. Thereby, the spherical aberration in the compensation lens unit can be reduced and the axial coma in camera shake compensation on the longer focal length side can be reduced. The condition (2) defines a condition therefor, and by fulfilling the condition (2), spherical aberration is excellently corrected. When the lower limit of the condition (2) is exceeded, spherical aberration increases toward the negative side. When the upper limit of the condition (2) is exceeded, spherical aberration increases toward the positive side.

Moreover, it is preferable that the zoom lens system according to the present invention has at least one concave lens element in its first lens unit, has at least one concave lens element in the negative front lens unit of its second lens unit, and fulfills the following condition (3): $$ - 0.7 < ( 0.7 × C 1 ⁢ M ) + C 2 ⁢ M Φ WIDE < 0 ( 3 )

where C 1M is a curvature of the object side surface of the concave lens element in the first lens unit, C 2M is a curvature of the object side surface of the negative concave lens element in the second lens unit, and φ Wide is a refractive power of the entire lens system at the shortest focal length condition.

Most of the effects of the first and second lens units on distortion on the shorter focal length side are caused by the influence of the curvatures C 1M and C 2M . When the power relationships are substantially the same, distortion is not largely affected by another factor such as curvature. The off-axial image point movement error depends on the effect of the distortion generated in the first lens unit and the effect of the distortion generated in the second lens unit. The effect of the distortion of the first lens unit on the off-axial image point movement error is approximately 70% the effect of the distortion of the second lens unit on the off-axial image point movement error.

To excellently correct the off-axial image point movement error, the condition (3) is fulfilled. When the lower limit of the condition (3) is exceeded, the effect of the strongly negative lens element concave to the object side increases, so that large negative distortion increases the off-axial image point movement error toward the positive side. When the upper limit of the condition (3) is exceeded, negative off-axial image point movement error caused by a rotation of an object surface (described later in calculation with aberration coefficients) cannot be corrected.

Subsequently, a definition of aberration degradation in a camera shake compensating optical system like that of the present invention will be described with reference to FIGS. 13A to 13 D. The decentering aberrations (off-axial image point movement error, one-side blur, axial coma and axial lateral chromatic aberration) shown in the figures cause the image degradation of the camera shake compensating optical system.

Off-axial Image Point Movement Error {FIG. 13 A}

In a decentered optical system, a distortion due to the decentering is generated in addition to the normal distortion. For this reason, in a camera shake compensating optical system, when camera shake is compensated for so that the axial (in the center of the image plane) image point completely stops, the off-axial image point does not completely stop to cause an image blur. In FIG. 13A , reference numeral 1 represents a film plane, reference numeral 2 represents an image point in the compensated condition (post-decentering condition), reference numeral 3 represents an image point in the standard condition (pre-decentering condition), and reference numeral 4 represents a direction of camera shake compensation.

When the optical axis is along the X-axis, the camera shake direction is along the Y-axis (i.e. a camera shake compensation direction 4 is also along the Y-axis) and Y(y′, z′, θ′) is a Y coordinate (always y(0, 0, θ)=0 since camera shake is compensated for so that the axial image point completely stops) of the actual image point of a light beam with a paraxial image point (y′, z′) at a compensation angle θ, the following expression (a) holds:

ΔY(y′, z′, θ)=Y(y′, z′, θ)−Y(y′, z′, 0)  (a)

Unless specifically indicated, an off-axial image point movement error ΔY Y ′ with respect to the image point on the Y-axis and an off-axial image point movement error ΔY Z ′ with respect to the image point on the Z-axis are represented by the following expressions (b) and (c):

ΔY Y ′={ΔY(0.7field, 0, 0.7°)+ΔY(−0.7field, 0, 0.7°)}/2  (b)

ΔY Z ′=ΔY(0, 0.7field, 0.7°)  (c)

where 0.7field is approximately 15 mm in 35 mm film.

One-side Blur {FIG. 13 B}

Referring to FIG. 13B , reference numeral 5 represents an image plane which is asymmetric with respect to an optical axis AX, and reference numeral 6 represents an image plane which is symmetric with respect to the optical axis. Because of the asymmetry of the optical system, the image plane 5 is asymmetric with respect to the optical axis AX. Consequently, a meridional one-side blur ΔM′ and a sagittal one-side blur ΔS′ are represented by the following expressions (d) and (e), respectively:

ΔM′={meridional value (y′=0.7field, z=0, θ=0.7°)-meridional value (y′=−0.7field, z=0, θ=0.7°)}/2  (d)

ΔS′={sagittal value (y′=0.7field, z=0, θ=0.7°)-sagittal value (y′=−0.7field, z=0, θ=0.7 0 )}/2  (e)

Axial Coma {FIG. 13 C}

Referring to FIG. 13C , reference numeral 7 represents an axial luminous flux, and reference numeral 8 represents an axial principal light beam. As shown in the figure, the axial luminous flux 7 is not symmetric with respect to the axial principal light beam 8 , so that coma is generated. An axial coma AXCM generated at the axial luminous flux 7 is represented by the following expression (f):

 AXCM={Y(upper zonal, θ=0.7°)+Y(lower zonal, θ=0.7°)}/2  (f)

Axial Lateral Chromatic Aberration {FIG. 13 D}

The image point, which shifts according to the difference in wavelength, shifts on the axial light beam when the optical system is asymmetric. The axial lateral chromatic aberration generated in the axial principal light beam is represented by the following expression (g):

(axial lateral chromatic aberration)={Y(g-line, θ=0.7°)−Y(d-line, θ=0.7°)}  (g)

With respect to the above-described decentering aberrations, an application method is shown in a paper “Theory of Tertiary Aberration of an Optical System Where Decentering Exits” by Mr. Matsui (JOEM, June, 1990). The method is suitable for a case where a normal taking lens is decentered due to an attachment error. However, it cannot be directly applied to a camera shake compensating optical system where a co-axial relationship among the object plane, the taking lens and the image plane is shifted. In order that the method of the paper can be directly applied to the camera shake compensating optical system, the actual aberrations of the camera shake compensating optical system are represented by tertiary aberration coefficients by performing the subsequently-described conversion of expressions.

Application of Decentering Aberration Coefficients to Camera Shake Compensating Optical System

Referring to FIG. 14 showing a relationship between the optical system and coordinates, how to obtain the decentering aberration coefficients will be described. First, the expressions are defined as follows: $$ tan ⁢   ⁢ ω · cos ⁢   ⁢ φω = Y g ⁢   ⁢ $ $$ tan ⁢   ⁢ ω · sin ⁢   ⁢ φω = Z g ⁢   ⁢ $ $$ R · cos ⁢   ⁢ φ ⁢   ⁢ R = g ⁢   ⁢ $ g · Y * ⁢ R · sin ⁢   ⁢ φ ⁢   ⁢ R = g ⁢   ⁢ $ g · Z *

where g and g$ are an entrance pupil surface and the distance from the object side principal plane to an object plane (object surface) OS, respectively, ω is an angle of a straight line between the object point and the object side principal point H, to a reference axis and φω is its azimuth, and R is a radius of entrance pupil converted on the object side principal plane and φR is its azimuth.

Image point movement amounts ΔY and ΔZ on an image plane (image surface) IS when a vth surface from the object side is parallelingly decentered by a slight amount Eν in the Y direction relative to the reference axis are represented by the following expressions (1A) and (1B):

ΔY=−(Eν/2α k ′)·[(ΔE)ν+(N·tan ω) 2 ·{(2+cos 2φω)·(VE 1 )ν−(VE 2 )ν}

+2R·(N·tan ω)·{(2 cos(φR−φω)+cos(φR+φω))·(IIIE)ν+cos φR·cos φω·(PE)ν}+R 2 ·(2+cos 2φR)·(IIE)ν]  (1A)

ΔZ=−(Eν/2α k ′)·[(N·tan ω) 2 ·sin 2φω)·(VE 1 )ν+2R·(N·tan ω)·{sin(φR+φω)·(IIIE)ν+sin φR·sin φω·(PE)ν}+R 2 ·sin 2φR·(IIE)ν]  (1B)

Here, when (ΔE)ν is a prismatic effect (lateral shift of the image), (VE 1 )ν and (VE 2 )ν are rotationally asymmetric distortions, (IIIE)ν and (PE)ν are a rotationally asymmetric astigmatism and an inclination of the image surface, respectively, and (IIE)ν is a rotationally asymmetric coma which is present also on the axis, the decentering aberration coefficients representing the effects of the decentering are represented by the following expressions (1C) to (1H) based on the aberration coefficients of from the vth surface to the image surface (# is a suffix representative of “on the object surface”). In the case of rotational decentering, the decentering aberration coefficients are represented by expressions similar to the expressions (1A) to (1H):

(ΔE)ν=−2(αν′−αν)  (1C)

(VE 1 )ν=[{αν′·(μ=ν+1 →k )ΣVμ}−{αν·(μ=ν→ k )ΣVμ}]−[{αν′#·(μ=ν+1 →k )ΣIIIμ}−{αν#·(μ=ν→ k )ΣIIIμ}]  (1D)

(VE 2 )ν={αν′#·(μ=ν+1 →k )ΣPμ}−{αν#·(μ=ν→ k )ΣPμ}  (1E)

(IIIE)ν=[{αν′·(μ=ν+1 →k )ΣIIIμ}−{αν·(μ=ν→ k )ΣIIIμ}]−[{αν′#·(μ=ν+1 →k )ΣIIμ}−{αν#·(μ=ν→ k )ΣIIμ}]  (1F)

(PE)ν={αν′·(μ=ν+1 →k )ΣPμ}−{αν·(μ=ν→ k )ΣPμ}  (1G)

(IIE)ν=[{αν′·(μ=ν+1 →k )ΣIIμ}−{αν·(μ=ν→ k )ΣIIμ}]−[{αν′#·(μ=ν+1 →k )ΣIμ}−{αν#·(μ=ν→ k )ΣIμ}]  (1H)

However, in order to apply the decentering aberration coefficients to the camera shake compensating optical system, it is necessary to replace the image surface IS with the object surface OS by a reversal of the optical system to use aberration coefficients from the image surface IS. That is, the image point movement amounts must be converted to those of the object surface OS. The reasons therefor will be described.

The first reason is that the light beam passing position sometimes shifts due to decentering. Referring to FIG. 15A (L 1 represents a light beam before decentering and L 2 represents a light beam after decentering), according to the above-described method of Mr. Matsui's paper, the light beam passing position on the image surface IS side of a decentering lens LS is shifted by the decentering lens LS. Consequently, the aberration coefficients of the decentering lens LS and of the decentering lens LS to the image surface IS relate to the decentering aberration coefficients. On the contrary, referring to FIG. 15B (M 1 represents a light beam before camera shake compensation and M 2 represents a light beam after camera shake compensation), in the camera shake compensating optical system (ideally), the light beam passing position on the object side of the decentering lens LS differs between before camera shake compensation and after camera shake compensation. Consequently, the aberration coefficients of the decentering lens LS and the lenses located on the object side of the decentering lens LS relate to the decentering aberration coefficients.

The second reason is that the aberrations sometimes degrade due to a rotational conversion of the object surface. According to the above-described method of Mr. Matsui's paper, neither the object surface OS 1 nor the image surface IS moves, whereas in the camera shake compensating optical system, the object surface OS 1 rotates as shown in FIG. 16 . For this reason, the off-axial image point movement error and the one-side blur are great compared to the case where the object surface does not rotate. In FIG. 16 , OS 1 represents an object surface before camera shake compensation and OS 2 represents an object surface after camera shake compensation.

Aberration Coefficients of Reversal Optical System and Aberration Coefficients of Non-reversal Optical System

Since the image point movement amounts must be converted to those of the object surface for the above-described reasons, the coefficients of the expressions (1A) to (1H) are converted according to the following expressions (2A) to (2J) represented based on FIG. 17 (non-reversal optical system):

R α= R N/ R g$=−α′ . . . (2A)

R α#=α′# . . . (2B)

R αμ′=−αν . . . (2C)

R αμ′#=αν# . . . (2D)

R Pμ=Pν . . . (2E) . . . same

R φμ=φν . . . (2F) . . . same

R Iμ=Iν . . . (2G) . . . same

R IIμ=−IIν . . . (2H) . . . reverse

R IIIμ=IIIν . . . (2I) . . . same

R Vμ=−Vν . . . (2J) . . . reverse

where R ( ) represents a reversal optical system and N is a refractive index.

Decentering Aberration Coefficients and Camera Shake Aberration Coefficients when Compensating Lens Unit Parallely Decenters

Since the previously-mentioned expressions (1A) to (1H) show a case where only one surface ν is decentered, they are converted to expressions showing a case where a plurality of surfaces i to j are decentered. When the compensating lens unit is parallel decentered, since the decentering amounts Ei to Ej of the decentered surfaces i to j are the same, the aberration coefficients can be treated as a sum as shown in the following expression:

(ΔE) i to j =(ν= i→j )Σ{−2·(αν′−αν)}

From αν′=αν+1, the following expression is obtained:

(ΔE) i to j =−2·(α j′−αi )

Likewise, with respect to other aberration coefficients, the terms between Σs are deleted. For example,

(PE) i to j =(μ= i→j )Σ{αν′·(μ=ν+1 →k )ΣPμ−αν·(μ=ν→ k )ΣPμ}

 =α j ′·(μ= j +1 →k )ΣPμ−α i ·(μ= i→k )ΣPμ

This is further converted to

(PE) i to j =(α j′−αi )·(μ= j +1 →k )ΣPμ−α i ·(μ= i to j )ΣPμ

where (μ=j+1→k)ΣPμ is the sum of P (Petzval) of the lenses arranged behind the compensating lens unit, and (μ=i to j)ΣPμ is the sum of P of the compensating lens unit.

(PE) i to j =(α j′−αi )P R −αi ·P D

where ( ) R is the sum of the aberration coefficients of the lenses arranged behind the compensating lens and ( ) D is the sum of the aberration coefficients of the compensating lens unit. The symbol of parentheses ( ) with a sub-script is a shorthand notation to indicate that an appropriate character or string of characters can be included in place of this mathematical notation.

As described above, by the conversion of the image point movement amounts to those of the object surface and the conversion of the expressions to the expressions showing the case where a plurality of surfaces i to j are decentered, the decentering aberration coefficients represented by the following expressions (3A) to (3F) are obtained. By re-defining the decentering aberration coefficients according to the expressions (3A) to (3F), the expressions (1A) to (1H) can be used as they are as expressions representing the image point movement amounts on the object surface.

(ΔE) i to j =−2·(α j′−αi )  (3A)

(VE 1 ) i to j =(α j′−αi )·V R −(α j′#−αi #)·III R −(α i ·V D −αi #·III D )  (3B)

(VE 2 ) i to j =(α j#−αi #)·P R −αi #·P D   (3C)

(IIIE) i to j =(α j′−αi )·III R −(α j′#−αi #)·II R −(α i ·III D −αi #·II D )  (3D)

(PE) i to j =(α j′−αi )·P R −αi ·P D   (3E)

(IIE) i to j =(α j′−αi )·II R −(α j′#−αi #)·I R −(α i ·II D −αi #·I D )  (3F)

Off-axial Image Point Movement Error

Subsequently, the off-axial image point movement error will be described. The decentering aberration coefficients (of the reversal optical systems) are represented by ΔE, VE 1 , VE 2 , IIIE, PE and IIE. The movements of the image point (before rotational conversion on the object surface) due to decentering on the object surface are represented by the following expressions (4A) and (4B) (in the principal light beam (R=0)). The expressions (4A) and (4B) are the expressions (1A) and (1B) where R=0.

ΔY#=−(E/2α′ k )·[ΔE+(N·tan ω) 2 ·{(2+cos 2 φω)VE 1 −VE 2 }]  (4A)

ΔZ#=−(E/2α′)·{(N·tan ω) 2 ·sin 2φω·VE 1 }  (4B)

Based on the expressions (4A) and (4B), the following expressions (4C) and (4D) are obtained (axial light beam, tan ω=0):

ΔY o #=−(E/2α′ k )·ΔE  (4C)

 ΔZ o #=0  (4D)

Subsequently, the rotational conversion will be described with reference to FIGS. 18A and 18B . From FIG. 18A , the following expression holds:

Y#= g $ k ·tan ω

From the sine theorem,

Y′#/{sin(π/2−ω′)}=(Y#+ΔY#−ΔY o #)/{sin(π/2+ω′−θ)}

ΔY′# after the rotational conversion is represented by the following expression:

ΔY′#=(Y′#)−(Y#)

 =[Y#·cos ω′+{(ΔY#)−(ΔY 0 #)}cos ω′−Y#·cos(ω′−θ)]/cos(ω′−θ)

Only the numerators of this expression are converted.

[Y#·cos ω′+{(ΔY#)−(ΔY 0 #)}·cos ω′−Y#·cos(ω′−θ)]

 =Y#·cos ω′+{(ΔY#)−(ΔY 0 #)}·cos ω′−Y#·cos θ·cos ω′−Y#·sin θ·sin ω′

 =(1-cos θ)·Y#·cos ω′+{(ΔY#)−(ΔY o #)}·cos ω′−Y#·sin θ·sin ω′

Here, since θ is small and ignorable compared to the other values, (1−cos θ)=θ 2 /2, sin θ=θ, and cos ω′/{cos(ω′−θ)}=1, sin ω′/{cos(ω′−θ)}=tan ω.

Therefore, the following expression is obtained:

ΔY′#=(ΔY#−ΔY o #)−Y # ·θ·tan ω

(ΔY#−ΔY o #) represents the off-axial image point movement error of parallel decentering and Y#·θ tan ω is an additional term (irrelevant to the aberration coefficients) due to rotation. Since ω at this time is on an X-Y cross section,

ΔY′#=(ΔY#−ΔY o #)−Y#·tan ω·cos φω  (5A)

Subsequently, the conversion to the image surface IS will be described with reference to FIG. 19. A magnification β is represented by the following expression:

β= g $ 1 /g $ k =α k ′/α 1

where α 1 =1/g$ 1 . The relationship between the image surface IS and the object surface OS is represented by the following expression:

Y=β·Y#

Y# and ΔY# which take the form of /α k ′×( ) are converted as follows:

Y=β·Y#

 =(α k ′/α 1 )·(1/α k ′)×( )

 = g $ 1 ×( )

Here, if g$ k ′→∞, g$ 1 −F 1 . Therefore, the following expression holds:

Y=−F 1 ×( )

 =−F 1 ×α k ′×Y #

Subsequently, the off-axial image point movement error on the image surface will be described. From the expression (4C) and α k ′=1/g k ′$, a decentering amount E is represented by the following expressions:

θ=ΔY 0 #/g $ k ′=E·ΔE/2

E=2·θ/ΔE

Normalization is performed so that the camera shake compensation angle θ is constant (0.7 deg=0.0122173 rad).

By performing parallel decentering (rotational decentering is not performed) to image-surface-convert ΔY=(ΔY#−ΔY 0 #) (here, N·tan ω=/F 1 , Φ 2 =Y 2 +Z 2 ), the following expressions (6A) to (6D) are obtained:

 ΔY=(θ·Φ 2 /F 1 )·[{2+cos 2·φω)·VE 1 −VE 2 }/ΔE]  (6A)

ΔZ=(θ·Φ 2 /F 1 )·[{(sin 2·φω)·VE 1 −VE 2 }/ΔE]  (6B)

Y + image point, Y − image point {φω=0, π of the expressions (6A) and (6B)}:

ΔY Y =(θ·Y 2 /F 1 )·{(3·VE 1 −VE 2 )/ΔE}  (6C)

Z image point {φω=π/2 of the expressions (6A) and (6B)}

ΔY Z=(θ·Z 2 /F 1 )·{(VE 1 −VE 2 )/ΔE}  (6D)

Then, rotational conversion is performed. Since Y#=−Y/(F 1 ×α k ′), with respect to −Y#·θ·tan ω·cos φω of the expression (5A), the following expression holds:

−Y#·θ·tan ω·cos φω=Y/(F 1 ×α k ′)·θ·tan ω·cos φω

At the Y + image point and the Y − image point, since φω=0, π and tan ω/α k ′=Y, −Y#·θ·tan ω·cos φω on the image surface is −Y#·θ·tan ω·cos φω=Y 2 ·θ/F 1 . By adding this to the expression (6C), the following expression (6E) is obtained. At the Z image point, since φω=π/2, −Y#·θ·tan ω·cos φω on the image surface is −Y#·θ·tan ω·cos φω=0. By adding this to the expression (6D), the following expression (6F) is obtained:

ΔY Y ′=(θ·Y 2 /F 1 )·{(3·VE 1 −VE 2 −ΔE)/ΔE}  (6E)

ΔY Z ′=ΔY Z   (6F)

One-side Blur

Subsequently, the one-side blur will be described. From the expressions (1A) and (1B), ΔM is {(primary term of R) of ΔY φR=0}×g$ k ′ and ΔS is {(primary term of R) of ΔZ φR=π/2}×g$ k ′. Before rotation, the following expression holds on the object surface OS (here, α k ′=N k ′/g$ k ′ and E/2=θ/ΔE are used):

ΔM#=(− g $ k ′ 2 ·θ/N k ′)×2·R·(N·tan ω)·cos φω·{(3·IIIE+PE)/ΔE}

After the rotation, the following expression holds:

 ΔM′#≈ΔM#+θY#

By converting the aberration coefficients to those on the image surface and substituting N k ′=1 and N=1, the following expression is obtained:

ΔM′=β 2 ·αM′#

 =− g $ 1 2 ·θ×2·R·tan ω·cos φω·{(3·IIIE+PE)/ΔE}+β·Y·θ

If the object surface OS is ∞ (here, g$,=−F 1 , β→0, tan ω=Y/F 1 and φω=0), the following expression (7A) representative of a meridional one-side blur ΔM′ is obtained. Likewise, an expression (7B) representative of a sagittal one-side blur is obtained.

ΔM′=−2·F 1 ·Y·θ·R·{(3·IIIE+PE)/ΔE}  (7A)

ΔS′=−2·F 1 ·Y·θ·R·{(IIIE+PE)/ΔE}  (7B)

Axial Coma

Subsequently, axial coma will be described. Based on the expression (1A), coma by ω=0 and upper decentering is represented by the following expression:

ΔY Upper #=ΔY#(ω=0, φ R =0)−ΔY#(ω=0, R=0)

 =−E/(2·α′)×R 2 ×3·IIE

Coma by ω=0 and lower decentering (the same as ΔY Upper # including the sign) is represented by the following expression:

ΔY Lower #=ΔY # (ω=0, φ R =π)−ΔY#(ω=0, R=0)

 =−E/(2·α′)×R 2 ×3·IIE

Since ω=0, axial coma is hardly varied by the rotational conversion. By the conversion from the object surface OS to the image surface IS (ΔY=β·ΔY#, E/2=θ/ΔE), the following expression is obtained

ΔY Upper =F 1 ×θ×R 2 ×(3·IIE/ΔE)=ΔY Lower

The axial coma AXCM is represented by the following expression (8A):

AXCM=(ΔY Upper +ΔY Lower )/2

 =ΔY Upper   (8A)

A part of each of the expressions (6E), (6F), (7A), (7B) and (8A) is newly defined as an aberration coefficient represented by the following expressions (9A) to (9E):

Off-axial image point movement error of the image point on the Y-axis . . . VE Y ={( 3·VE 1 −VE 2 −ΔE)/ΔE}  (9A)

Off-axial image point movement error of the image point on the Z-axis . . . VE Z ={( VE 1 −VE 2 )/ΔE}  (9B)

Marginal one-side blur . . . IIIE M ={(3·IIIE+PE)/ΔE}  (9C)

Sagittal one-side blur . . . IIIE S ={(IIIE+PE)/ΔE}  (9D)

Axial coma . . . IIE A {(3·IIE)/ΔE}  (9E)

By substituting the expressions (3A) to (3F) in the expressions (9A) to (9B) representative of the camera shake aberration coefficients, the following expressions (10A) to (10E) representative of camera shake aberration coefficients are obtained:

VE Y =−½·{3V R −3V D ·A+ 2 −(3·III R +P R )·H#+(3·III D +P D )·A#}  (10A)

VE Z =−½·{V R −V D ·A−(III R +P R )·H#+(III D +P D )·A#}  (10B)

IIIE M =−½·{(3·III R +P R )−(3·III D +P D )·A−3·II R H#+3·II D ·A#}  (10C)

IIIE S =−½·{(III R +P R )−(III D +P D )·A−II R ·H#+II D ·A#}  (10D)

IIE A =−3/2·(II R +II D ·A−I R ·H#+I D ·A#)  (10E)

where ( ) D is the sum of the aberration coefficients of the compensating lens unit;

( ) R is the sum of the aberration coefficients of the lens units arranged behind (on the object side of) the compensating lens unit;

A=αi/(αj′−αi) (here, the compensating lens units are i to j), A#=αi#/(αj′−αi); and

H#=(αi′#−αi#)/(αj′−αi).

ΔE=−2·(αj′−αi) (here, (αj′−αi) is ±0.0122173 when 0.70°/mm) which is the coefficient of (camera shake compensation angle)/(decentering amount) aims substantially at a predetermined value (however, the sign differs according to whether the compensating lens units are positive or negative). Therefore, A is an incident angle of a marginal light beam to the compensating lens units (viewed from the image side) and A# is proportional to the incident angle of the principal light beam. When h# and h do not vary so much in the compensating lens units, H# represents a ratio between h# of the principal light beam and h of the marginal light beam.

Since the decentering aberration coefficients in the expressions (10A) to (10E) are defined as those of the reversal optical system, it is necessary to return them to the coefficients of the non-reversal optical system. Returning the coefficients in the expressions (10A) to (10E) by using the expressions (2A) to (2J), the following expressions (11A) to (11E) are obtained:

VE Y =+½·{3V F −3V D ·A−2+(3·III F +P F )H#−(3·III D +P D )·A#}  (11A)

VE Z =+½·{V F −V D ·A+(III F +P F )H#−(III D +P D )·A #}   (11B)

 IIIE M =−½·{(3·III F +P F )−(3·III D +P D )·A+3·II F ·H#−3·II D ·A#}  (11C)

IIIE S =−½·{(III F +P F )−(III D +P D )·A+II F ·H#II D ·A#}  (11D)

IIE A =+3/2·(II F −II D ·A+I F ·H#−I D ·A # )  (11E)

where ( ) D is the sum of the aberration coefficients of the compensating lens units and the reversal optical system;

( ) F is the sum of the aberration coefficients of the lens units arranged in front of the compensating lens units;

A=−α n ′/(α n′−αm );

A#=α n ′#/(α n−αm );

H=−(α n#−αm #)/(α n′−αm )=−(Σ h μ#·φμ)/(Σ h μ·φμ); and

ΔE=−2(α n′−αm ) (compensating lens units: m→n , non-reversal lens system: j←i ).

From the expressions (11A) to (11E), the following are understood: First, as described previously, while the decentered lens unit and the lens units arranged therebehind relate to the performance according to the method of Mr. Matsui's paper, the decentered lens unit and the lens units arranged therebefore relate to the performance in the expressions (11A) to (11E). Secondly, the off-axial image point movement error tends to increase in wide angle optical systems (the focal length F 1 of the compensating lens unit is the denominator) and one-side blur and axial coma tend to increase in telephoto optical systems.

Thirdly, although the degradation of aberrations due to decentering decreases by reducing the aberration coefficients of the decentered lens unit and the lens units arranged there-before, a constant (−2 in { } of the expression (11A)) remains in the coefficient VE Y of the off-axial image point movement error ΔY Y ′. This is a term generated since the object surface OS and the image surface IS incline relative to each other due to rotational camera shake. The off-axial image point movement error due to the constant term (−2) is remarkably great in wide angle optical systems. For example, the off-axial image point movement error ΔY Y ′=−72 μm at a focal length F 1 of 38 mm, which is not ignorable. The off-axial image point movement error due to the constant term (−2) remains even if the aberration coefficients are 0. Therefore, it is preferable to set the aberration coefficients so that the constant term (−2) is canceled. The condition (3) is a condition therefor.

Fourthly, in order to reduce the aberration degradation due to decentering, it is necessary to reduce the aberration coefficients and the coefficients such as A, A# and H# multiplied by the aberration coefficients. With respect to A and A#, the denominator α n ′−α m is reduced. However, since this is directly connected to ΔE=−2(α n ′−α m ), if it is too great, the camera shake compensation sensitivity (how many degrees the luminous flux is bent at when the lens is decentered by predetermined millimeters) is too high, so that a mechanical driving accuracy is necessary. With respect to H#, the closer the compensating lens unit is to the aperture stop, the smaller h# of each surface is, so that H# is also small.

Numerical data of the first and second embodiments of the present invention are shown in Tables 1 and 2. In the tables, ri (i=1,2,3, . . . ) represents a radius of curvature of an ith surface from the object side, di (i=1,2,3, . . . ) represents an ith axial distance from the object side (here, the axial distances of the camera shake compensating lens before decentering are shown), Ni (i=1,2,3, . . . ) and νi (i=1,2,3, . . . ) represent a refractive index and an Abbe number to the d-line of an ith lens element from the object side, respectively. f represents the focal length of the entire lens system. FNo. represents the F-number.

In the tables, the surfaces marked with asterisks are aspherical and defined by the following expression representative of the configuration of an aspherical surface: $$ X = C · Y 2 1 + ( 1 - ε · Y 2 · C 2 ) 1 2 + ∑ i ⁢ AiY i

where X is an amount of displacement from the reference surface along the optical axis, Y is a height in a direction vertical to the optical axis, C is a paraxial curvature, ε is a conic constant, and Ai is an ith aspherical coefficient.

FIGS. 1 and 2 respectively show the lens arrangements of the first and second embodiments at the shortest focal length condition (W). Arrows m 1 , m 2 and m 3 schematically show the movements of a first lens unit Gr 1 , a second lens unit Gr 2 and an aperture stop S, and a third lens unit Gr 3 from the shortest focal length condition (W) to the longest focal length condition (T).

The first embodiment comprises from the object side: a first lens unit Gr 1 including a negative meniscus lens element concave to the object side and a positive bi-convex lens element; a second lens unit Gr 2 (hatched portion) including a negative meniscus lens element (negative front lens unit) concave to the image side and a positive meniscus lens element (positive rear lens unit) convex to the image side; an aperture stop S; and a third lens unit Gr 3 including a positive meniscus lens element convex to the image side and a negative meniscus lens element concave to the object side. The following surfaces are aspherical: both side surfaces of the negative meniscus lens element of the second lens unit Gr 2 ; and both side surfaces of the positive meniscus lens element of the third lens unit Gr 3 .

The second embodiment comprises from the object side: a first lens unit Gr 1 including a negative meniscus lens element concave to the image side and a positive meniscus lens element convex to the object side; a second lens unit Gr 2 (hatched portion) including a negative front lens unit including a negative bi-concave lens element and a positive bi-convex lens element, and a doublet lens element (positive rear lens unit) consisting of a negative meniscus lens element concave to the image side and a bi-convex lens element; and aperture stop S; and a third lens unit Gr 3 including a positive meniscus lens element convex to the image side and a negative meniscus lens element concave to the object side. The following surfaces are aspherical: both side surfaces of the biconcave lens element of the second lens unit Gr 2 ; the image side surface of the doublet lens element of the second lens unit Gr 2 ; and both side surfaces of the positive meniscus lens element of the third lens unit Gr 3 .

FIGS. 3A to 3 F and 4 A to 4 F show longitudinal aberrations of the first and second embodiments in the standard condition (pre-decentering condition) at the shortest focal length condition (W) ( FIGS. 3A to 3 C and 4 A to 4 C) and at the longest focal length condition (T) ( FIGS. 3D to 3 F and 4 D to 4 F). The solid lines d represents aberration to the d-line. The broken line SC represents sine condition. The broken line DM and the solid line DS represent astigmatism on the meridional image plane and astigmatism on the sagittal image plane, respectively.

FIGS. 5A to 5 E through 8 A to 8 E show lateral aberrations of the second lens unit Gr 2 of the first embodiment before decentering ( FIGS. 5A , 5 B, 6 A, 6 B, 7 A, 7 B, 8 A and 8 B) and after decentering ( FIGS. 5C to 5 E, 6 C to 6 E, 7 C to 7 E and 8 C to 8 E). FIGS. 9A to 9 E through 12 A to 12 E show lateral aberrations of the second lens unit Gr 2 of the second embodiment before decentering ( FIGS. 9A , 9 B, 10 A, 10 B, 11 A, 11 B, 12 A and 12 B) and after decentering ( FIGS. 9C to 9 E, 10 C to 10 E, 11 C to 11 E and 12 C to 12 E). FIGS. 5C to 5 E, 6 C to 6 E, 7 C to 7 E, 8 C to 8 E, 9 C to 9 E, 10 C to 10 E, 11 C to 11 E and 12 C to 12 E show aberrations in a condition where compensation is made at a camera shake compensation angle θ=0.7 deg. (=0.0122173 rad). FIGS. 5A to 5 E, 6 A to 6 E, 9 A to 9 E and 10 A to 10 E show lateral aberrations at the shortest focal length condition (W). FIGS. 7A to 7 E, 8 A to 8 E, 11 A to 11 E and 12 A to 12 E show lateral aberrations at the longest focal length condition (T). FIGS. 5A to 5 E, 7 A to 7 E, 9 A to 9 E and 11 A to 11 E show lateral aberrations with respect to a luminous flux on the meridional image plane. FIGS. 6A to 6 E, 8 A to 8 E, 10 A to 10 E and 12 A to 12 E show lateral aberrations with respect to a luminous flux on the sagittal image plane. The symbol Y′ represents an image height or an imaging position on the image plane with respect to a zero point that is situated on the intersection between an optical axis and the image plane. The value of Y′ in the respective figures throughout the specification is explanatory of the aberrations to a person of skill in this field.

Table 3 shows values corresponding to the conditions (1) to (3) with respect to the first and second embodiments. Table 4 shows aberration degradation (i.e. error amounts in a parallel decentered condition) of the first and second embodiments in camera shake compensation at the shortest focal length condition (W) and at the longest focal length condition (T).

Thus, in the embodiments of the present invention, although the magnification is as high as 3 to 4×, the aberration degradation is small in the entire zoom range from the shortest to the longest focal length conditions even if the compensating lens unit is decentered for camera shake compensation. In addition, the embodiments of the present invention are suitable for use in lens shutter cameras since they are compact.

As described above, according to the zoom lens system having a camera shake compensating function according to the present invention, by using for camera shake compensation the second lens unit serving as a zooming lens unit, the generation of decentering aberration is restrained while required compactness is maintained. Moreover, by arranging the second lens unit to have a negative, positive power configuration and arranging the aperture stop behind the second lens unit, the off-axial image point movement error and the one-side blur can excellently be compensated for. Further, by increasing the distance between the first and second lens unit to perform zooming from the shorter focal length side to the longer focal length side, chromatic aberration is excellently corrected. Thus, even in a zoom lens system with a magnification of 3× or higher, camera shake compensation is made while required compactness is maintained and high optical performance is maintained in the entire zoom range.

In addition, since distortion is excellently corrected by fulfilling the condition (1) and spherical aberration is excellently corrected by fulfilling the condition (2), optical performances both before and after the compensation are improved.

Obviously, many modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood that within the scope of the appended claims, the invention may be practiced other than as specifically described.

TABLE 1
(1st Embodiment)
f = 38.9 to 112.7   FNo. = 4.12 to 10.06
	Radius of	Axial	Refractive	Abbe
	Curvature	Distance	Index	Number
	r1	−23.134
	d1	1.480	N1	1.80500	ν1	40.97
	r2	−43.384
	d2	0.691
	r3	84.476
	d3	3.947	N2	1.48749	ν2	70.44
	r4	−28.730
	d4	1.974 to 19.858
	r5*	37.755
	d5	2.862	N3	1.84506	ν3	23.66
	r6*	29.619
	d6	1.974
	r7	−37.076
	d7	3.257	N4	1.51680	ν4	64.20
	r8	−11.740
	d8	2.566
	r9	∞ (Aperture stop)
	d9	14.277 to 1.776
	r10*	−93.451
	d10	3.454	N5	1.58340	ν5	30.23
	r11*	−29.294
	d11	3.651
	r12	−12.159
	d12	0.987	N6	1.78850	ν6	45.68
	r13	−98.834
Σd = 41.119 to 46.502
	Aspherical Coefficients
	r5: ε = 1.0000
	A4 = −0.17862 × 10 −3
	A6 = −0.16659 × 10 −5
	A8 = −0.38927 × 10 −8
	A10 = 0.44900 × 10 −10
	A12 = −0.16019 × 10 −11
	r6: ε = 1.0000
	A4 = −0.13469 × 10 −3
	A6 = −0.14553 × 10 −5
	A8 = 0.13468 × 10 −7
	A10 = −0.11665 × 10 −9
	A12 = −0.10306 × 10 −11
	A14 = 0.67707 × 10 −15
	A16 = 0.60892 × 10 −16
	R10: ε = 1.0000
	A3 = −0.37915 × 10 −3
	A4 = 0.20239 × 10 −3
	A5 = −0.40425 × 10 −4
	A6 = 0.44402 × 10 −5
	A7 = 0.77130 × 10 −7
	A8 = −0.46861 × 10 −7
	A9 = −0.43276 × 10 −9
	A10 = 0.33181 × 10 −9
	A11 = 0.80295 × 10 −11
	A12 = −0.22144 × 10 −11
	A13 = −0.39322 × 10 −14
	A14 = −0.37118 × 10 −17
	r11: ε = 1.0000
	A3 = −0.31594 × 10 −3
	A4 = 0.72536 × 10 −4
	A5 = −0.11831 × 10 −4
	A6 = −0.18478 × 10 −7
	A7 = 0.54421 × 10 −7
	A8 = 0.44369 × 10 −7
	A9 = −0.91140 × 10 −8
	A10 = 0.12688 × 10 −9
	A11 = 0.50618 × 10 −10
	A12 = −0.17558 × 10 −12
	A13 = −0.23579 × 10 −12

TABLE 2
(2nd Embodiment)
f = 38.2 to 147.0   FNo. = 3.55 to 9.57
	Radius of	Axial	Refractive	Abbe
	Curvature	Distance	Index	Number
	r1	29.916
	d1	1.571	N1	1.84666	ν1	23.82
	r2	23.932
	d2	0.687
	r3	23.477
	d3	4.517	N2	1.51680	ν2	64.20
	r4	69.470
	d4	3.928 to 33.619
	r5*	−30.365
	d5	1.277	N3	1.76683	ν3	49.47
	r6*	21.645
	d6	1.964
	r7	25.792
	d7	2.602	N4	1.83350	ν4	21.00
	r8	−259.608
	d8	1.915
	r9	25.444
	d9	1.669	N5	1.83350	ν5	21.00
	r10	12.325
	d10	4.822	N6	1.51178	ν6	69.07
	r11*	−14.971
	d11	1.080
	r12	∞ (Aperture stop)
	d12	21.121 to 2.875
	r13*	−41.831
	d13	3.634	N7	1.84506	ν7	23.66
	r14*	−24.936
	d14	3.044
	r15	−14.963
	d15	1.178	N8	1.75450	ν8	51.57
	r16	−2311.924
Σd = 55.010 to 66.456
	Aspherical Coefficients
	r5: ε = 1.0000
	A4 = −0.10080 × 10 −3
	A6 = 0.17197 × 10 −5
	A8 = −0.17247 × 10 −7
	A10 = 0.82125 × 10 −10
	A12 = −0.72093 × 10 −12
	r6: ε = 1.0000
	A4 = −0.52707 × 10 −4
	A6 = 0.15108 × 10 −5
	A8 = 0.33309 × 10 −8
	A10 = −0.17757 × 10 −9
	A12 = 0.60417 × 10 −14
	R11: ε = 1.0000
	A4 = 0.12379 × 10 −4
	A6 = 0.59111 × 10 −6
	A8 = −0.40424 × 10 −7
	A10 = 0.97489 × 10 −9
	A12 = −0.90941 × 10 −11
	r13: ε = 1.0000
	A4 = 0.17108 × 10 −4
	A6 = −0.28707 × 10 −6
	A8 = 0.57772 × 10 −8
	A10 = −0.48868 × 10 −10
	A12 = 0.16153 × 10 −12
	r14: ε = 1.0000
	A4 = −0.45301 × 10 −5
	A6 = −0.31847 × 10 −6
	A8 = 0.56666 × 10 −8
	A10 = −0.47316 × 10 −10
	A12 = 0.13749 × 10 −12

	TABLE 3
	1st embodiment	2nd embodiment
$$ φ I φ W	0.325	0.320
φ DF	−0.00516	−0.02076
C DR	−0.08518	−0.06680
$$ φ DF C DR	0.06057	0.31077
$$ ( 0.7 × C 1 ⁢ M ) + C 2 ⁢ M Φ WIDE	−0.147	−0.365

	TABLE 4
	1st embodiment	2nd embodiment
	W	T	W	T
	Off-axial image point	−0.010	0.002	0.007	0.001
	movement error: ΔY y ′
	Off-axial image point	0.033	0.013	0.035	0.011
	movement error: ΔY z ′
	Meridional one-side	−0.156	−0.172	−0.166	0.102
	blur: ΔM′
	Sagittal one-side	0.075	0.329	0.036	0.596
	blur: ΔS′
	Axial coma: AXCM	−0.002	−0.019	−0.001	−0.029
	Axial lateral	0.008	0.023	0.002	0.019
	chromatic aberration

Claims

1. A zoom lens system consisting from an object side:a first lens unit of a positive refractive power; a second lens unit of a positive refractive power movable in a vertical direction relative to an optical axis for compensation of an image blur caused by vibration of the entire zoom lens system, said second lens unit consisting of three or less lens elements; and a third lens unit of a negative refractive power; wherein said first through third lens units are movable in an optical axis direction for zooming from a shortest focal length condition to a longest focal length condition so that a distance between said first and second lens units increases and a distance between said second and third lens units decreases, wherein a most image side surface of the second lens unit is convex to an image side and the following condition is fulfilled: 0.03<φDFCDR<0.5 where φDF is a refractive power of a front lens unit of the second lens unit and CDR is a curvature of the most image side surface of the second lens unit.

2. A zoom lens system as claimed in claim 1, wherein the following condition is fulfilled: 0<φIφW<0.57where φI is a refractive power of the first lens unit and φW is a refractive power of the entire zoom lens system at a shortest focal length condition.

3. A zoom lens system consisting from an object side:a first lens unit of a positive refractive power; a second lens unit of a positive refractive power movable in a vertical direction relative to an optical axis for compensation of an image blur caused by vibration of the entire zoom lens system, said second lens unit consisting of three or less lens elements; and a third lens unit of a negative refractive power, wherein said first through third lens units are movable in an optical axis direction for zooming from a shortest focal length condition to a longest focal length condition so that a distance between said first and second lens units increases and a distance between said second and third lens units decreases, wherein the second lens unit consisting of from the object side, a front lens unit of a negative refractive power including a negative lens element and a rear lens unit of a positive refractive power including a negative lens element, wherein the following condition is fulfilled: -0.7<(0.7×C1⁢M)+C2⁢MΦWIDE<0where C1M is a curvature of an object side surface of a negative lens element of the first lens unit, C2M is a curvature of an object side surface of a negative lens element of the second lens unit and ΦWIDE is a refractive power of the entire zoom lens system at a shortest focal length condition.

4. A zoom lens system as claimed in claim 3, wherein the following condition is fulfilled: 0<φIφW<0.57where φI is a refractive power of the first lens unit and φW is a refractive power of the entire zoom lens system at a shortest focal length condition.

5. A zoom lens system consisting from an object side:a first lens unit of a positive refractive power; a second lens unit of a positive refractive power movable in a vertical direction relative to an optical axis for compensation of an image blur caused by vibration of the entire zoom lens system; an aperture stop; and a third lens unit of a negative refractive power, wherein said first through third lens units are movable in an optical axis direction for zooming from a shortest focal length condition to a longest focal length condition so that a distance between said first and second lens units increases and a distance between said second and third lens units decreases wherein a most image side surface of the second lens unit is convex to an image side and the following condition is fulfilled: 0.03<φDFCDR<0.5 where φDF is a refractive power of a front lens unit of the second lens unit and CDR is a curvature of the most image side surface of the second lens unit.

6. A zoom lens system as claimed in claim 5, wherein the following condition is fulfilled: 0<φIφW<0.57where ΦI is a refractive power of the first lens unit and ΦW is a refractive power of the entire zoom lens system at a shortest focal length condition.

7. A zoom lens system as claimed in claim 5, wherein the second lens unit consisting of from the object side, a front lens unit of a negative refractive power including a negative lens element and a rear lens unit of a positive refractive power including a negative lens element, wherein the following condition is fulfilled: -0.7<(0.7×C1⁢M)+C2⁢MΦWIDE<0where C1M is a curvature of an object side surface of a negative lens element of the first lens unit, C2M is a curvature of an object side surface of a negative lens element of front lens unit of the second lens unit.

8. A zoom lens system as claimed in claim 5, wherein said second lens unit consists of from the object side:a front lens unit of a negative refractive power; and a rear lens unit of a positive refractive power.

9. A zoom lens system consisting of from an object side:a first lens unit of a positive refractive power; a second lens unit of a positive refractive power movable in a vertical direction relative to an optical axis for compensation of an image blur caused by vibration of the entire zoom lens system, said second lens unit consisting of a front lens unit of a negative refractive power and a real lens unit of a positive refractive power; and a third lens unit of a negative refractive power, wherein said first through third lens units are movable in an optical axis direction for zooming from a wide-angle condition to a telephoto condition so that a distance between said first and second lens units increases and a distance between said second and third lens units decreases, wherein the following condition is fulfilled: 0.03<ΦDF/CDR<0.5  where ΦDF is a refractive power of the first lens unit of the second lens unit and CDR is a curvature of the most image side surface of the second lens unit.

10. A zoom lens system as claimed in claim 9, wherein the following condition is fulfilled:0<φ1/φW<0.57 where φ1 is a refractive power of the first lens unit and φW is a refractive power of the entire zoom lens system at a shortest focal length condition.

11. A zoom lens system as claimed in claim 9, wherein the following condition is fulfilled: -0.7<(0.7×C1⁢M)+C2⁢MΦWIDE<0wherein C1M is a curvature of an object side surface of a negative lens element of the first lens unit, C2M is a curvature of an object side of a negative lens element of the front lens unit of the second lens unit.

12. A zoom lens system consisting of from an object side:a first lens unit of a positive refractive power; a second lens unit of a positive refractive power movable in a vertical direction relative to an optical axis for compensation of an image blur caused by vibration of the entire zoom lens system, said second lens unit consisting of a front lens unit of a negative refractive power and rear lens unit of a positive refractive power; an aperture stop; and a third lens unit of a negative refractive power, wherein said first through third lens units are movable in an optical axis direction for zooming from a wide angle condition to telephoto condition so that a distance between said first and second lens units increases and a distance between said second and third lens units decreases, wherein the following condition is fulfilled: 0.03<ΦDF/CDR<0.5  where ΦDF is a refractive power of the front lens unit of the second lens unit and CDR is a curvature of the most image side surface of the second lens unit.

13. A zoom lens system as claimed in claim 12, wherein the following condition is fulfilled:0<φ1/φW<0.57 where φ1 is a refractive power of the first lens unit and φW is a refractive power of the entire zoom lens system at a shortest focal length condition.

14. A zoom lens system as claimed in claim 12, wherein the following condition is fulfilled: -0.7<(0.7×C1⁢M)+C2⁢MΦWIDE<0wherein C1M is a curvature of an object side surface of a negative lens element of the first lens unit, C2M is a curvature of an object side surface of a negative lens element of the front lens unit of the second lens unit.