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Backstepping control of aircraft take-off in windshear
IFAC-PapersOnLine. 2019. Vol. 52. No. 16. P. 712–717.
Golubev A., Botkin N. D., Krishchenko A. P.
In this paper, we deal with the problem of aircraft take-off control in the presence of a windshear. A simplified point mass nonlinear model of aircraft dynamics assuming the flight in a vertical plane is used. A reference trajectory is constructed to satisfy the altitude, relative path inclination and relative velocity state constraints. An integrator backstepping based control design procedure using barrier Lyapunov functions is suggested to track the constructed reference trajectory under state constraints and windshear disturbances.
Language:
English
Panov V., Ryabchenko A., / Series arXiv "stat.ME". 2026. No. 2607.05048.
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Golubev A., Glazkov T. V., , in: Proceedings of the Workshop on Mathematical Modeling and Scientific Computing: Focus on Complex Processes and Systems — dedicated to the memory of Nikolai Botkin (MMSC 2020).: CEUR Workshop Proceedings, 2020. Ch. 2783 P. 113–127.
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Botkin N. D., Golubev A., Turova V. L., IFAC-PapersOnLine 2019 Vol. 52 No. 16 P. 706–711
The problem of aircraft take-off under windshear conditions is considered as a differential game. A simplified five-dimensional nonlinear model of aircraft dynamics, assuming the flight in a vertical plane, is used. The overloads, differences between the projections of the thrust and drag, respectively lift, forces are considered as control variables. The corresponding technically relevant control, ...
Added: November 18, 2021