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- W2615697087 abstract "In the paper the design of an aircraft flight controller based on the Dynamic Contraction Method is presented. The control task is formulated as a tracking problem of aerodynamic state variables: velocity of flight and flight path angle, which are responsible for aircraft flight conditions in the longitudinal movement. The applied DCM method allows to create the expected outputs for non-linear and non-stationary objects in spite of incomplete information about varying parameters of the system and external disturbances. The proposed technique is tested by simulations of a few maneuvers under wind gust for a F-16 aircraft model." @default.
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- W2615697087 date "2003-06-01" @default.
- W2615697087 modified "2023-09-24" @default.
- W2615697087 title "Longitudinal Directional flight Control Design Using Robust Dynamic Contraction Method" @default.
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- W2615697087 doi "https://doi.org/10.1016/s1474-6670(17)35688-4" @default.
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