Application to Aircraft Control During Landing

2007

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DOI 10.1007/978-0-8176-4553-3_4
Data confidence 70 medium
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Abstract

An approach for constructing a robust feedback control for problems having linear dynamics with disturbances is suggested.Auseful control is assumed to be scalar and bounded.The approach can be applied to conflict-controlled systems, where the constraint for the disturbance is unknown in advance. Adjustment of the method is based on results of the theory of linear differential games with fixed terminal time and geometric constraints for the players’ controls.The algorithm for constructing the robust control is fulfilled as a computer program for the case when the quality of the process is defined only by two components of the phase vector at the terminal instant. The paper presents simulation results for the problem of lateral motion control of an aircraft during landing under wind disturbance.