Description
In the case of the Su-27, the pilot initially disengages the angle of attack limiter of the plane, normally set at 26°. This action also disengages the g limiter. After that the pilot pulls back on the stick hard. The aircraft reaches 90–120° angle of attack with a slight gain of altitude and a significant loss of speed. When the elevator is centered, the drag at the rear of the plane causes torque, thus making the aircraft pitch forward. At that time the pilot adds power to compensate for the lift loss. In a properly performed Pugachev's Cobra, the plane maintains almost straight flight throughout the maneuver; the plane does not roll or yaw in either direction. Proper entry speed is significant because, if entering at too low a speed, the pilot might not be able to accomplish the maneuver; entering at too high a speed might result in airframe damage due to the high g-force or for the pilot to lose consciousness.
While Pugachev's Cobra can be executed using only standard aerodynamic controls, it could be achieved more easily with modern thrust vectoring. In the latter case it would be an example of supermaneuverability, specifically poststall maneuvering. The Herbst maneuvering and the helicopter manoeuvre are other examples of the recent growing use of vectored thrust in 4.5 and 5th generation aircraft, manned as well as unmanned.
Read more about this topic: Pugachev's Cobra
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