Synthesis of the Optimal Control of an Axisymmetric Rotating Aircraft with Using a Spiral Forecast ModeL

This article presents mathematical models of the dynamics of an aircraft stabilized by rotation. The optimal control algorithm is developed according to the A.A. Krasovsky criterion with such a real-time motion apparatus using a spiral forecast model in combination with a proportional-integral-differential (PID) controller. The results of numerical simulation are presented, showing the applicability of the approach used to the considered class of aircraft.