Method of Synthesis of the Adaptive Noise-Immune Roll Angle Autopilot

The problem of synthesizing the adaptive system for an aircraft roll angle automatic control, which ensures the uniformity of the object control in all flight modes using a combined self-adjusting loop, is considered. It is shown that the developed adaptive autopilot makes it possible to ensure the noise immunity of the roll channel under the action of stepwise and random disturbances. The simulation results are presented.