exemplary embodiments now will be described more fully hereinafter with reference to the accompanying drawings , in which exemplary embodiments are shown . this disclosure may , however , be embodied in many different forms and should not be construed as limited to the exemplary embodiments set forth therein . rather , these exemplary embodiments are provided so that this disclosure will be thorough and complete , and will fully convey the scope of this disclosure to those skilled in the art . in the description , details of well - known features and techniques may be omitted to avoid unnecessarily obscuring the presented embodiments . the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of this disclosure . as used herein , the singular forms “ a ”, “ an ” and “ the ” are intended to include the plural forms as well , unless the context clearly indicates otherwise . furthermore , the use of the terms a , an , etc . does not denote a limitation of quantity , but rather denotes the presence of at least one of the referenced item . the use of the terms “ first ”, “ second ”, and the like does not imply any particular order , but they are included to identify individual elements . moreover , the use of the terms first , second , etc . does not denote any order or importance , but rather the terms first , second , etc . are used to distinguish one element from another . it will be further understood that the terms “ comprises ” and / or “ comprising ”, or “ includes ” and / or “ including ” when used in this specification , specify the presence of stated features , regions , integers , steps , operations , elements , and / or components , but do not preclude the presence or addition of one or more other features , regions , integers , steps , operations , elements , components , and / or groups thereof . unless otherwise defined , all terms ( including technical and scientific terms ) used herein have the same meaning as commonly understood by one of ordinary skill in the art . it will be further understood that terms , such as those defined in commonly used dictionaries , should be interpreted as having a meaning that is consistent with their meaning in the context of the relevant art and the present disclosure , and will not be interpreted in an idealized or overly formal sense unless expressly so defined herein . in the drawings , like reference numerals in the drawings denote like elements . the shape , size and regions , and the like , of the drawing may be exaggerated for clarity . from a robotics standpoint , the variable view image system can be realized by a camera - robot system with eye - in - hand configuration , where a camera is mounted on a robot &# 39 ; s end effector . as shown in the fig1 , the view state can be defined as a vector : here , ( x w , y w ) is the view position . the view orientation ( γ , φ ) is composed of the azimuth angle γ and the zenith angle φ . the world coordinate frame o w x w y w z w and the local coordinate frame o v x v y v z v are defined , as shown in fig1 . in the world coordinate frame , the x w y w plane is located at the object plane of the system . the local coordinate frame o v x v y v z v is fixed on the observed target . the azimuth angle γ and zenith angle φ are defined with respect to the local coordinate frame o v x v y v z v . in korean patent application no . 10 - 0839871 , the rotation angle of the scanning mirror 21 and view angle are coupled as shown in fig2 . the zenith angle decrease in order to observe the object in the center of the object plane . to decouple the rotation angle of the scanning mirror and view angles , a telecentric scanner is designed and introduced to the system , which includes a two axis scanning mirror 21 and a telecentric lens group 20 . the system layout is shown in fig3 . the view position can be steered by the telecentric scanner . the view direction can be steered by double wedge prisms 10 and 11 . a first intermediate image is formed by a first imaging optical element 31 . optical elements 32 and 33 integrate a deformable mirror 40 into the system . the deformable mirror 40 is used for correction of aberration induced by the wedge prisms . the optical elements 34 and 33 relay the active aperture of the deformable mirror to the system aperture . a final imaging optical element 35 forms a final image on the image sensor 60 . the concept of the telecentric system is shown in fig4 , where the telecentric lens group is simplified as a lens 20 . a stop 70 is located at the focal point of the telecentric lens . it makes an entrance pupil infinitely . therefore in the object side , the chief rays are always parallel to the optical axis . when the telecentric lens is integrated to the system , the scanning mirror is located at the focal point of the telecentric lens . the azimuth angle and zenith angle of view are only related to the rotation angle of the prisms . the telecentric scanner is designed separately from the whole system . a preliminary design for the experiment setup is shown in fig5 . diffraction limit is achieved in the design . a two axis scanner includes an x axis scanning mirror 210 and a y axis scanning mirror 211 . a telecentric lens group consists of two lenses , a plano - convex lens 200 and an achromatic doublet lens 201 . the maximum peak - valley wavefront error of the whole system including wedge prisms is less than 2 . 6 λ ( λ = 660 nm ). the zenith and azimuth variation with the change of the scanning mirror angle when θ p1 = θ p2 =− 90 ° is shown in fig6 ( a ) and ( b ). as can be seen , the zenith angle φ equals 18 . 9 °. the azimuth angle γ equals 90 °. the motion of the scanning mirror and view orientation are decoupled . and a larger zenith angle is achieved . during the operation of the system , the angle of wedge prism and scanning mirror can be determined based on the kinematics and jacobian matrix of the system . the kinematics of the system can be defined as : where ( x w , y w , φ , λ ) is the vector for work space variables . the position ( x s , y s ) of ray after the telecentric lens group can be defined by the following equations : x s = d tan ( θ sx )/ cos ( θ sy )+ a tan ( θ sx ) where d is the distance between the principal plane of the telecentric lens group and the y scanning mirror 211 . a is the distance between the two mirrors . the configuration of two mirror scanning system is shown in fig7 . the ray tracing of the wedge prisms is shown in fig8 . by applying ray tracing through each surface , the final azimuth angle γ , zenith angle φ , and the view position ( x w , y w ) can be determined by the following equations : φ = cos − 1 ( x 5 ( 3 )); γ = π − a tan 2 ( x 5 ( 1 ), x 5 ( 2 )); where x 5 is the vector of ray between the last surface of the second wedge prism 11 and the object plane . e 5 is the cross point between x 5 and the object plane . in actual operation of the system , determination of joint variables given the position and orientation of view is more important . the relationship between the joint space and working space is nonlinear and complex . an analytical inverse relationship is difficult to obtain . therefore a numerical solution to inverse kinematics is applied in the present invention . the jacobian of the system can be divided to four parts as shown as follows : because of the decoupled design , the inverse jacobian can be expressed as : ( 1 ) desired working space variable is set as v d =[ x w , d y w , d γ d φ d ]′. ( 2 ) initial joint variables are p 0 =[ x s y s θ p1 θ p2 ] t 0 . where λ r and λ t are the gain factors . δ is the damping factor . δ = δ 0 ( 1 − ω / ω 0 ) 2 , if ω & lt ; ω 0 ; otherwise , δ = 0 , where ω =√{ square root over ( det ( jj t ))}. ( 5 ) if v d − f ( p i + 1 )& lt ; ε , then p i is the result , else go to ( 3 ). although the integration of active components in the present invention can achieve new functions , it also introduces aberrations that can degrade the quality of the image . in the present invention , a deformable mirror device 40 is applied to correct the aberration . instead of using a wavefront sensor , the system calculates the focus measure of the image captured from the camera . the control system uses focus measure as metric to represent the aberration of the image . the control signal is generated to change the surface of the deformable mirror iteratively during operation . as can be seen , because no wavefront sensor or laser source is used , the present invention becomes simple and robust to different kind of targets . the control diagram is shown in fig9 . in order to compare the present invention with the earlier approach with the coupled design , one simulation result is shown in fig1 . both systems apply double wedge prisms with 18 ° 8 ′ vertex angle . in the initial state , the top view of micro gear can be achieved from both systems . fig1 ( a ) shows the top view of a micro gear . because of self - occlusion , the hole in the gear cannot be observed . in order to observe the hole in the gear , a view with maximum zenith angle needs to be achieved . the current system can change the zenith angle φ up to 18 . 9 °. the captured image is shown in fig1 ( b ), where the hole in the gear can be observed . however , the earlier approach with the coupled design can only achieve the zenith angle φ up to 13 . 8 °. the captured image is shown in fig1 ( c ). as can be seen , a larger area of interest is achieved in the present system . the ability of the present invention to change the view without moving the object was tested using multi views of a micro chip . the top view of the micro chip is shown in fig1 ( a ), when θ sx = 0 °, θ sy =− 0 . 37 °, θ r1 = 180 ° and θ r2 = 0 °. the zenith angle φ is 0 . 43 °. the side of the chip cannot be observed due to self - occlusion . using a conventional optical system , it is difficult to observe every side of an object . however , in the present invention , by changing the configuration of the prisms and the scanning mirror , images with a different zenith angle φ and azimuth angle γ can be achieved . fig1 ( b ) shows the view with a zenith angle φ = 18 . 9 ° and an azimuth angle γ = 0 ° when θ sx =− 1 . 16 °, θ sy = 0 °, θ r1 = 90 ° and θ r2 = 90 °. the left side of the chip and the solder joint can be observed . fig1 ( c ) shows the view with a zenith angle φ = 18 . 9 ° and an azimuth angle γ = 90 ° when θ sx = 0 °, θ sy = 1 . 28 °, θ r1 = 0 ° and θ r2 = 0 °. fig1 ( d ) shows the view with a zenith angle φ = 18 . 9 ° and an azimuth angle γ = 270 ° when θ sx = 1 . 16 °, θ sy = 0 °, θ r1 =− 90 ° and θ r2 =− 90 °. fig1 ( e ) shows the view with a zenith angle φ = 18 . 9 ° and an azimuth angle γ = 270 ° when θ sx = 0 °, θ sy =− 1 . 28 °, θ r1 =− 180 ° and θ r2 =− 180 °. the dash lines indicate that every side of the chip can be observed with a different configuration of the wedge prisms and the scanning mirror . as can be seen , the present invention can obtain more vision information compared to a conventional optical system . as the scanning mirror also changes the zenith angle , the maximal zenith angle is different at different view positions . a microassembly application is shown in fig1 . the micro shaft needs to be inserted into the hole of the micro gear as shown in fig1 ( a ). fig1 ( b ) shows the top view of the micro gear and micro shaft . from the top view , the micro shaft can be moved near the micro gear first as shown in fig1 ( c ). however , it is impossible to make an insertion without information about the hole in the gear . with the present invention , the system can change the zenith angle and azimuth angle of view to 18 . 9 ° and − 90 °. the captured image in this configuration is shown in fig1 ( d ). then , the micro shaft can be aligned with the hole as shown in fig1 ( e ). the present system has a simple kinematics . the inverse kinematics is easy to get a solution , which is important for automation of the system . the zenith angle of view can achieve a large value compared to the previous system , which can provide more vision information when occlusion happens . while the exemplary embodiments have been shown and described , it will be understood by those skilled in the art that various changes in form and details may be made thereto without departing from the spirit and scope of this disclosure as defined by the appended claims . in addition , many modifications can be made to adapt a particular situation or material to the teachings of this disclosure without departing from the essential scope thereof . therefore , it is intended that this disclosure not be limited to the particular exemplary embodiments disclosed as the best mode contemplated for carrying out this disclosure , but that this disclosure will include all embodiments falling within the scope of the appended claims .