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Mathematical modeling shows optimal control enhances aircraft dynamics, indicating effective stabilization methods.
The article presents mathematical models of the dynamics of an aircraft stabilized by rotation. An optimal control algorithm has been developed according to the A. A. criterion. Krasovsky with such a realtime motion apparatus using a spiral forecast model in combination with a PID controller. The results of numerical simulation are presented, showing the applicability of the approach used to the considered class of aircraft.
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E. A. Znamenskiy (2025) studied this question.
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