Identification of Engine Thrust and Aerodynamic Drag Force According to Flight Test Data with Smoothing of Random Measurement Errors von Korsun, O. N., Poplavsky, B. K., Stulovskii, A. V., Om, Moung Htang

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Direct Method for Forming the Optimal Open Loop Control of Aerial Vehicles von Korsun, O. N., Stulovskii, A. V.

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Comparative Study of Pontryagin Maximum Principle and Direct Method in Aircraft Optimal Control Design von Korsun, O N, Stulovskii, A V, Gulevich, S P

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Identification of Aerodynamic Coefficients of Longitudinal Movement and Error Estimates for Onboard Measurements of Supercritical Angles of Attack von Kanyshev, A. V., Korsun, O. N., Ovcharenko, V. N., Stulovskii, A. V.

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Aircraft aerodynamic coefficients identification using flight tests data von Korsun, O N, Stulovskii, A V, Balyk, O A, Zolotaeva, M V

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Methods for selecting the supporting curve for the model of hysteresis loop von Korsun, O.N., Stulovskii, A.V.

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Algorithms of increasing the calculation accuracy for an aircraft’s orientation angle von Bulgakov, V. V., Korsun, O. N., Kulabukhov, V. S., Stulovskii, A. V., Timofeev, D. S.

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Optimal Control Design for Maneuverable Aircraft Using Population-based Algorithms von Korsun, O.N., Sergeev, S.A., Stulovskii, A.V.

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Real-time Aerodynamic Parameter Identification for the Purpose of Aircraft Intelligent Technical State Monitoring von Korsun, O.N., Om, M.H., Latt, K.Z., Stulovskii, A.V.

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Smoothing of Aircraft On-Board Measurements Based on the Use of Flight Dynamics Equations and Nonlinear Programming Methods von Korsun, O. N., Om, M. H., Stulovskii, A. V.

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Methods of Computing Thrust Vector Coordinates for Aircrafts Equipped With Thrust Vector Control von Kanyshev, Alexey V., Korsun, Oleg N., Stulovskii, Alexander V.

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