VESTNIK of Samara University. Aerospace and Mechanical EngineeringVESTNIK of Samara University. Aerospace and Mechanical Engineering2542-04532541-7533Samara National Research University63110.18287/2541-7533-2009-0-1(17)-30-40UnknownCommand control of hypersonic aircraft angle of attack during acceleration and climbKotchyanA. G.vest@ssau.ruSamara State Aerospace University1803200981304005062014Copyright © 2015, VESTNIK of the Samara State Aerospace University2015<p>The paper deals with the tasks of forming command control of hypersonic aircraft: the main aircraft and the accelerator aircraft during acceleration and climb. The motion is analysed in conditions of atmospheric density perturbations and deviations of aircraft aerodynamic characteristics. An algorithm of single-channel (by the angle of attack) direction is proposed and its ability to compensate the impact of perturbations on satisfying the final conditions of motion is investigated.</p>Hypersonic aircraftangle of attackperturbed motioncommand controlГиперзвуковой летательный аппаратугол атакивозмущённое движениекомандное управление