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ISSUE:    Almanac of Modern Science and Education. 2016. Issue 1
COLLECTION:    Technical Sciences

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METHODS TO SOLVE THE TASK OF TERMINAL OPTIMAL AIRCRAFT CONTROL TAKING INTO ACCOUNT THE CORRECTION OF INTEGRATED CONTROL

Stanislav Valer'evich Ivanov
Don State Technical University

Tat'yana Sergeevna Babenko
Don State Technical University

Anton Andreevich Reva
Don State Technical University

Andrei Aleksandrovich Bessmertnyi
Don State Technical University
Submitted: January 15, 2016
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
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References:
  1. Андреевский В. В. Динамика спуска космических аппаратов на Землю. М., 1970. 232 с.
  2. Бородовский В. Н., Лавров В. Н. Терминальное управление на атмосферном участке выведения // Ракетная техника: сборник. Сер. 5. 1973. Вып. 7 (9). С. 328-330.
  3. Сейдж Э. П., Уайт Ч. С. Оптимальное управление системами. М.: Радио и связь, 1982. 392 с.
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