ELECTROMECHANICAL ADAPTIVE CONTROL SYSTEMS FOR LONGITUDINAL MOTION OF AIRCRAFT, DEVELOPED BASED ON THE ADAPTIVE BYPASS METHOD OF THE INTEGRATOR
Deals with the development and research of adaptive electromechanical control systems for the longitudinal movement of aircraft of light and ultralight classes based on the adaptive bypass method of the integrator. Nonlinear mathematical models of the dynamics of the longitudinal movement of the aircraft are constructed, taking into account and not taking into account the electromagnetic dynamics of the executive electric elevator. The results of computer studies of the effectiveness of the constructed electromechanical adaptive systems in achieving the properties of dynamic stability and speed under the influence of electromagnetic dynamics are presented. The studies were carried out on the basis of the calculation model of the UAV-70V light unmanned aerial vehicle (weighing 65 kg) of the Aerospace Academy company (Vietnam), designed for remote monitoring of underlying surfaces.
Authors: V. V. Putov, V. N. Sheludko, D. M. Filatov, Chan Kuok Toan, Chu Trong Su
Direction: Electrical Engineering
Keywords: Aircraft, longitudinal movement, adaptive control, integrator bypass method, electromagnetic dynamics of executive electric drives
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