In order to realize the autonomous precision guidance of air defense missile,the system scheme of the IR imaging/Ladar dual-mode seeker with a common aperture was proposed,and the optical system used in was designed.It included two guidance modes,i.e.passive IR imaging mode and active ladar mode.The passive IR imaging system was used for searching and identifying target,and then was switched to the active ladar mode to lock and precisely track the target.The system had a common receiving aperture,and its structure was very compact,so it could meet the requirement for the miniaturization of the seeker.Besides,it also could meet the demands of a wide field of view for searching target,and the demands for accurately recognizing and tracking the target at the same time.So the dual field of view passive IR optics was demanded.In order to increase the narrow FOV tracking performance,the dual FOV infrared optical used the zooming mode which some components flip in or out the optical system to firm the target signal.Here the infrared camera was based on a Sofradirs 320?56 staring focal plane array detector,and operated at a constant relative aperture F/2 over the dual zoom range in wavelength of 3.7 to 4.8μm.The dual FOV optics are divided into the zooming part,with dual variable focal length,and the reimaging part which was chosen in such a way to minimize the objective lens while maintaining 100%cold shield efficiency.The final infrared optics including 4白3?NFOV)and 16白12?WFOV)was designed.The NFOV lens composed of two common IR/Ladar lens,three relay lens,a beam splitter and two reflective fold mirrors,while WFOV lens increased two lens such as Germanium and Silicon.The common IR/Ladar lens ZnS and ZnSe could refractive the IR optics and Laser optics.The beam splitter which refractived IR optics and reflected Laser optics was located in the middle of Germanium and Silicon.The designed optical system had good image quality,and fufiled the performance requirement of seeker system.