VELOCITY VECTOR CONTROL OF AIRCRAFT
Yu. N. Zolotukhin, K. Yu. Kotov, A. S. Mal’tsev, A. A. Nesterov, A. P. Yan
Institute of Automation and Electrometry, Siberian Branch, Russian Academy of Sciences, Novosibirsk, Russia
Keywords: flight speed control system, structural synthesis of nonlinear automatic systems
Abstract
In this paper we address the problem of velocity vector control of aircraft in the flight path axis system. The development of an automatic flight path control system requires reaching a desired flight speed with coordinated control of rudders and engine thrust. For that purpose the nonlinear controller based on method of structural synthesis is built. Simulation results of the complete closed-loop system demonstrate the effectiveness of the proposed approach.
|
