Abstract: A camera module includes: a first body including a substrate; an image sensor mounted on the substrate; a second body including a lens module; a ball bearing disposed between the first body and the second body to enable movement of the second body relative to the first body; and a driving member disposed between the first body and the second body to provide driving force to move the second body in at least one direction intersecting an optical axis.

Abstract: Disclosed herein is a system and method for simulating real-time visualizable electronic warfare. The system includes a location calculation unit for calculating location coordinates of the aircraft and the missile for each frame according to a display frame rate, a display unit for visualizing, for each frame, movement of the aircraft and the missile depending on the location coordinates thereof, a precise tracking unit for, when a relative distance between the aircraft and the missile is less than a dangerous distance, dividing an interval between a current frame and a subsequent frame into sub-intervals based on the display frame rate, and sampling locations of the aircraft and the missile, and a proximity fuse control unit for processing the missile to explode when a relative distance between sampled locations of the aircraft and the missile, is less than or equal to a maximum explosible distance of a proximity fuse of the missile.

Abstract: Disclosed herein is a system and method for simulating real-time visualizable electronic warfare. The system includes a location calculation unit for calculating location coordinates of the aircraft and the missile for each frame according to a display frame rate, a display unit for visualizing, for each frame, movement of the aircraft and the missile depending on the location coordinates thereof, a precise tracking unit for, when a relative distance between the aircraft and the missile is less than a dangerous distance, dividing an interval between a current frame and a subsequent frame into sub-intervals based on the display frame rate, and sampling locations of the aircraft and the missile, and a proximity fuse control unit for processing the missile to explode when a relative distance between sampled locations of the aircraft and the missile, is less than or equal to a maximum explosible distance of a proximity fuse of the missile.

Abstract: RF decoy anti-missile testing in a virtual environment through simulating the aviation of a missile, the reflected signal of a target, and an active RF decoy by use of a target motion simulator which implements the moving trajectory of the RF decoy. The RF decoy radiates a reflected signal of the target and also a deception signal through use of a microwave device that transfers the detected signal from the missile and amplifies the received signal so that a repeated delay signal of the RE decoy greater than that of the reflected signal of the target is radiated by the target motion simulator, thereby testing the deceit performance of the decoy.

Abstract: Disclosed is an active RF decoy simulation apparatus for simulating an active RF decoy system in virtual environment, comprising: a missile seeker which radiates RF signals and detects reflection signals from the target ship, a target motion simulator for implementing the moving trajectory of active RF decoy, in which an antenna for radiating the reflected signal of the target ship and another antenna for radiating the deception signal of the active RF decoy according to the transmitted missile signal are mounted, a microwave device which transfers the detected signal radiated from the missile to the antenna so that the reflected signal of the target ship is radiated by the target motion simulator and which receives the signal radiated from the missile, amplifies the received signal and transfers the signal to the antenna so that a repeated delay signal of the RF decoy simulator which is greater than the reflected signal of the target ship is radiated by the target motion simulator, a missile seeker control d