The invention discloses an anti-shock camera used for an aircraft. The anti-shock camera comprises a driving box, a universal shaft, a camera body, a battery storage shell, a loudspeaker and a detection controlling shell. The upper end of the battery storage shell is connected with the driving box through the universal shaft. The driving box is arranged at the bottom of an installation plate. The front end of the battery storage shell is in threaded connection with the detection controlling shell. The front end of the detection controlling shell is in threaded connection with a camera installation cover. The rear end of the battery storage shell is connected with the loudspeaker. The camera installation cover is of a circular structure. The camera body is installed in the circle center of the camera installation cover. According to the anti-shock camera used for the aircraft, shooting or photographing at different angles is achieved, and the flexibility is high; in addition, shooting can be conducted normally in a dim environment, and a good buffer function is achieved; furthermore, an alarm is given in time when vibration is large, early-warning is achieved, the camera body is prevented from being damaged, the stabilizing effect is good, the shooting quality is high, and installation, using and maintenance are convenient.