Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization

The paper deals with the task of optimizing a space vehicles trans-atmospheric motion in order to maximize its terminal velocity at prescribed finite values of the height and trajectory inclination angle. The angle of attack acts as control in a vehicles passive motion. To determine the optimal prog...

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Bibliographic Details
Main Authors: V. L. Balakin, S. A. Ishkov, A. A. Khramov
Format: Article
Language:English
Published: Samara National Research University 2017-11-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/5223/5075