OPTIMAL AIRCRAFT CONTROL WITH FULL PARAMETER AND STATUS INFORMATION

   This article examines the optimal control for a non-stationary linear object using the example of an aircraft with complete information about the parameters and state. The lateral movement of the aircraft under the conditions of disturbances is considered. The mathematical model of the considered control object is described by a system of fifth-order differential equations. Ailerons and elevator deflections act as controls. Expressions are obtained for optimal control and optimal value of the quality functional. The simulation results of the investigated control system in Simulink, which is part of the Matlab package, confirm the effectiveness of optimal control for the problem of aircraft stabilization if the parameters and state of the object are fully known. The graphs of transient processes for the components of the state vector are obtained.

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