Abstract
A procedure for the structural synthesis of control algorithms and the calculation of their parameters is stated. It is demonstrated by theoretical analysis and the mathematical simulation of control process dynamics that the synthesized algorithms can implement an assigned dynamic behavior in systems and provide for their stability during parametric and coordinate disturbances.
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References
Krut’ko, P.D., Automation Control of Takeoff and Landing of Single-Rotor Helicopters, Problemy mashinostroeniya i nadezhnosti mashin, 2008, no. 3, pp. 90–99.
Krut’ko, P.D., Obratnye zadachi dinamiki v teorii avtomaticheskogo upravleniya. Tsikl lektsii (Dynamics Inverse Problems in the Theory of Automatic Control. Lecture Course), Moscow: Mashinostroenie, 2004.
Belen’kii, I.M., Vvedenie v analiticheskuyu mekhaniku (Introduction to Analytical Mechanics), Moscow: Vysshaya shkola, 1964.
Additional information
Original Russian Text © P.D. Krut’ko, 2009, published in Problemy Mashinostroeniya i Mashin, 2009, No. 5, pp. 90–100.
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Krut’ko, P.D. Algorithms of take-off and landing termination control for single-rotor helicopters. J. Mach. Manuf. Reliab. 38, 492–500 (2009). https://doi.org/10.3103/S105261880905015X
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DOI: https://doi.org/10.3103/S105261880905015X