Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria

Abstract

Constraint-driven method of GTE management optimization based on aircraft efficiency criteria is described. The method is based on dynamic programming and minimax principle of optimality for objective function.

About the authors

A. Yu. Tkachenko

Samara State Aerospace University

Author for correspondence.
Email: tau@ssau.ru

Candidate of Science

Associate Professor at Aircraft Engine Theory Department

Russian Federation

V. S. Kuzmichev

Samara State Aerospace University

Email: kuzm@ssau.ru

Doctor of Science

Professor at Aircraft Engine Theory Department

Russian Federation

References

  1. Кузьмичев, В.С. Моделирование полета летательного аппарата в задачах оптимизации параметров рабочего процесса газотурбинных двигателей [Текст] / В.С. Кузьмичев, А.Ю. Ткаченко, В.Н. Рыбаков // Известия Самарского научного центра Российской академии наук. – 2012. – т.14, №2(2). – С.491-494.
  2. Андреева, Е.А. Вариационное исчисление и методы оптимизации [Текст]: учебное пособие для университетов / Е.А. Андреева, В.М. Цирулева – М.:Высш. шк., 2006. – 584 с.

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