| 摘要 |
PURPOSE: A thrust vectoring missile decoy device is provided to maximize a decoy effect because an airframe performs a decoy action while horizontally flying in an erect posture at a low speed by a thrust vectoring device. CONSTITUTION: A thrust vectoring missile decoy device comprises an airframe(110), a decoy module(130), a thrust vectoring device(150), a gyro sensor(195), and a control module(170). The airframe obtains a thrust through a jet engine(140) in the rear part. The decoy module is installed inside the aircraft and receives frequency signals of a missile of an enemy and amplifies the frequency signals and transmits decoy signals. A thrust vectoring device is installed in the rear part of the airframe and changes a thrust direction of the jet engine so that the airframe horizontally flies in an erect posture at a low speed. The gyro sensor is installed inside the airframe and electrically connected to the decoy module, the gyro sensor, and the thrust vectoring device. The control module operates the thrust vectoring device by receiving posture information of the airframe from the gyro sensor and operation information of the decoy module. |
