Adaptive control systems for maneuverable aircraft based on decoupling of rolling and yawing motions

The problem of ensuring a preset dynamic accuracy of an adaptive system that controls the lateral movement of a maneuverable aircraft is considered. This system decouples the rolling and yawing motions at high angles of attack. The method for selecting the parameters of adaptation algorithms in a searchless reference model-based adaptive system is developed. This method allows one to eliminate the dependence of adaptation processes on the input control action level and on coordinate and parametric disturbances, to improve the rate of adaptation processes, to ensure the required quality of the transients relative to the coordinate error, and, thus, to improve the accuracy of functioning of the adaptive control system.