Control synthesis by network operator method for spacecraft descent on the moon

A control synthesis problem for spacecraft descent to the given domain near the Moon is considered. Mathematical model of the spacecraft, initial states, and terminal conditions are given. The goal is to synthesize the control so that the spacecraft could obtain the terminal state from the given domain of initial state in limited time. The synthesized control is a multidimentional function that describes dependence of control from the state coordinates. In this paper to solve the control synthesis problem we use a new numerical method of network operator. An example of spacecraft descent is given. © 2017 Univelt Inc. All rights reserved.

Авторы
Редакторы
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Сборник материалов конференции
Издательство
Univelt Inc.
Номер выпуска
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Язык
Английский
Страницы
873-883
Статус
Опубликовано
Подразделение
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Ссылка
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DOI
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Номер
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Том
161
Год
2017
Организации
  • 1 Federal Research Center Computer Science and Control of Russian Academy of Sciences (RAS), 44, Vavilova str, Moscow, 119333, Russian Federation
  • 2 Department of Mechanics and Mechatronics, Peoples' Friendship University of Russia (RUDN University), 6, Miklukho-Maklaya str, Moscow, 117198, Russian Federation
Ключевые слова
Cobalt compounds; Dysprosium compounds; Numerical methods; Space flight; Spacecraft; Control synthesis; Initial state; Multidimentional functions; Network operator; Spacecraft descent; Terminal state; Sulfur compounds
Дата создания
19.10.2018
Дата изменения
19.10.2018
Постоянная ссылка
https://repository.rudn.ru/ru/records/article/record/5922/