Archive of Scientific Articles

Abstract. The article examines a method to control the maneuvering aircraft at the landing stage under the conditions of the indeterminacy of its steering function. The authors identify two stages while solving this task: at the first stage they find optimal integrated control, at the second one - provide control formation with a view to approximate (to adjust) the real process to the model one. On the basis of the findings the paper concludes that using the proposed procedure allows efficient solving the task of optimal aircraft control under the conditions of the substantial indeterminacy of its steering function.

Key words and phrases: летательный аппарат, аэродинамические качества, принцип текущего итерационного программирования, управление летательным аппаратом, система дифференциальных уравнений, движение аэродинамически управляемого летательного аппарата в атмосфере, aircraft, aerodynamic qualities, principle of current iterative programming, aircraft control, differential equation system, motion of aerodynamically controlled aircraft in atmosphere