FIELD: aviation.
SUBSTANCE: group of inventions relates to the traffic control of non-rigid aircraft (1) with the motor (2). Piloting control is implemented by the control system with measuring device (3A), located near the rear end (1R) of the aircraft. The device (3A) determines the orientation (θM) of the aircraft, as well as measures the angle (δθM) and linear (δyM) aircraft deformations at the point (M) near to the rear end. Based on the latest mentioned, the aircraft orientation is improved and the engine (2) orientation (β) is corrected.
EFFECT: increasing of the control accuracy, with the weakening of the requirements to the aircraft design stiffness.
4 cl, 5 dwg
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