The invention relates to a device for eliminating the flying lateral force of an aircraft at a
high angle of
attack, which comprises a thin film support frame and a retraction and extension mechanism. A retraction and extension seam is formed on a
skin over the front part of the head part of the aircraft; a hinge (12) is fixedly arranged at the
zenith of the head part in the aircraft, and the center of the hinge is positioned on the axial line of the aircraft; the thin film support frame is mounted in the aircraft, and the thin film support frame is positioned on the longitudinal symmetric plane of the aircraft; and the
zenith end of a triangle of the thin film support frame is connected with the hinge (12) at the
zenith of the head part of the aircraft, and can rotate around the center of the hinge (12). When the aircraft flies within the flying range of the
high angle of
attack, the thin film support frame is popped up, a film
chip realizes the self-excited vibration in
airflow, produces the unsteady flow around the film
chip and realizes the control of asymmetric vortex, thereby eliminating the lateral force; when the aircraft recovers the small
angle of attack state, the retraction and extension mechanism retracts the support frame into a front body of a
slender body. The device is applicable to the aircrafts with the head taper of less than 42 degrees and characterized by simple structure and reliable performance.