Abstract Methodology of constructing a stationary multichannel flow aerometric receiver using the effects of deceleration and throttling of an incoming airflow and their circular transformation in the yaw plane is considered. The mathematical models and algorithms for processing primary informative signals entering along the channels of speed, altitude, angles of attack and slip of the helicopter air data system constructed on the basis of the aerometric receiver being proposed are obtained.
Methodology of construction and models of informative signals for a stationary miltichannel flow aerometric receiver of the helicopter air data system
Russian Aeronautics (Iz VUZ) ; 53 , 4 ; 457-465
2010-12-01
9 pages
Article (Journal)
Electronic Resource
English