TOTAL ENERGY CONTROL OF AIRCRAFT LONGITUDINAL MOTION
S. A. Belokon, Yu. N. Zolotukhin, K.Yu. Kotov, A. S. Maltsev, A. P. Yan
Institute of Automation and Electrometry, Siberian Branch, Russian Academy of Sciences, Novosibirsk, Russia
Keywords: total energy control, simulation, longitudinal motion control, inverse models
Abstract
The creation of a system for controlling the longitudinal motion of aircraft based on the principle of the total energy control is considered. The structure of the control system is presented. It includes a core independently of aircraft calculating commands for deflecting the elevator and thrust obtained on the basis of the principle of inverse models. The control system is implemented for models of three aircraft with different aerodynamic configurations. The study of the quality of regulation is carried out using the numerical modeling method.
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