An automatic detection method of angle of attack error and its correction system
An automatic detection and angle-of-attack technology, which is applied in the field of aircraft avionics, can solve problems such as the lack of effective and fast inspection methods and correction methods for faults, the zero position deviation of the installation of the angle-of-attack sensor, and the deviation of the angle-of-attack indication error. Modify the effect of easy and fast operation, improve safety, and improve the accuracy of angle of attack indication
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[0038] Such as figure 1 As shown, the system architecture:
[0039] Including air data computer 1, airspeed tube 2, angle of attack sensor 3, display and control system 4, flight control system 5, and inertial navigation system 6.
[0040] The crosslinking signal is designed as follows:
[0041] The air data computer 1 receives the static pressure signal of the pitot tube 2 for converting the lifting speed; receives the local angle of attack signal of the angle of attack sensor 3 for calculating the true angle of attack before correction; Pass or break signal, be used for judging whether to deny high flight; Receive pitch angle θ, roll angle γ, heading angle of inertial navigation system 6 It is used to judge the attitude of the aircraft; it receives the stapling and zeroing signals from the display and control system 4, and is used for correcting or clearing the angle of attack error; it sends the current stapling value and automatic error checking to the display and contr...
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