FLIGHT CONTROL OF SENSORS IN THE CONTROL SYSTEM WITH FUNCTIONAL TESTING

摘要

We consider flight control facilities for basic sensors in the aircraft automatic flight control system, namely angular rate sensor, overload sensor and angle of attack sensor. For the mathematical model of a sensor in the form of an oscillating link with an additive error we proposed an algorithm of flight control with functional testing using a signal from the flight parameter being measured. We examine variants of realization, present recommendations for choosing the algorithm parameters and show its efficiency in detecting typical failures of an angular rate sensor.