The invention discloses a kinetics analog system for the landing of an asteroid probe. A target celestial body topography generation unit is in charge of reading topographical gross DEM (Dynamic Effect Model) data, surface physical parameter profiles, and surface feature profiles, and polygon three dimensional topographical data conforming with the target celestial body topographical features are generated by an algorithm; a shadow projection generation unit is in charge of calculating the position of the target celestial body relative to the sun and the incident angle of solar ray at the current analog time according to an ephemeris, and rendering to generate a shadow projection map; a navigation camera imaging analog unit is in charge of rendering to generate an image in accordance with the requirements of a camera according to the information of current camera parameters, positions, illumination parameters, and topographical texture; a data input and output unit is in charge of receiving and resolving the data of the camera position, attitude parameters and current analog time sent over by a client side according to a protocol, meanwhile packaging and sending the image data generated by rendering to the client side according to the protocol so as to be used in the resolution of an autonomous optical navigation system, thus realizing the imaging analog of the navigated target.