Methods for designing adaptive autopilot controllers for aircraft based on speed, altitude, and overload.

Abstract

The invention relates to a method for designing an adaptive autopilot controller for aircraft (AES) that responds to velocity, altitude, and overload, consisting of two parts: Part I: determining the initial controller; Part II: determining the adaptive controller. The method eliminates the zero point of the transfer function, prevents continuous integration, and limits the control signal to ensure the operating conditions of the control loops. The use of a common control structure allows for the design and adjustment of control coefficients to be the same across all three channels, thereby generalizing the control problem. The solution ensures good adaptability to a wide range of flight scenarios for AES, especially AES with high velocity and overload, and continuously changing altitude.

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