SYNTHESIS OF AIRCRAFT MOTION CONTROL LAWS USING AGGREGATIVE CONTROLLER ANALYTICAL DESIGN PROCEDURE DURING AUTOMATIC INFLIGHT REFUELING

摘要

The report is aimed to solve the problem ofautomatization of in-flight aircraft refueling.The stated above process is quite complicatedand requires extremely precise flying skills fromthe pilot. As for the motion control system, itshall be very accurate and flexible. The reportcontains the solution to the tasks of autopilotsynergic synthesis to enable control of motion ofthe aircraft being refueled at the stage of finalapproach and fuel-feed line drogue capture. Thesynthesized adaptive controllers ensure highpositioning accuracy including compensation offorce and wind disturbances taking intoconsideration aircraft mass variation duringfuel servicing.