Nguen Viet Fiong, V. Putov, A. Putov, Chan Kuok Toan
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Abstract
This paper describes an adaptive control system of an air vehicle's (AV) longitudinal motion with account for wing aeroelasticity. A nonlinear mathematical model of resilient aircraft's longitudinal motion is designed. Adaptive control system of a resilient AV is built by means of majorizing function and its efficiency undergoes computerized testing under function parameter uncertainty of AV model and wind perturbations.
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