КФУ. Карточка публикации. ANALYSIS OF A MOTION MODEL OF ORBITAL TETHER SYSTEMS BASED ON PROPERTIES OF LIMIT CYCLES

КАЗАНСКИЙ
ФЕДЕРАЛЬНЫЙ УНИВЕРСИТЕТ

RUS

- EN
- 中文
- ES

ANALYSIS OF A MOTION MODEL OF ORBITAL TETHER SYSTEMS BASED ON PROPERTIES OF LIMIT CYCLES

Форма представления

Зарубежные монографии

Год публикации

2017

Язык

английский

Авторы, сотрудники КФУ

Воронцова Валерия Леонидовна, автор

Другие авторы

Druzhinina Olga Valentinovna, автор

Библиографическое описание на языке оригинала

Valeriya Vorontsova. ANALYSIS OF A MOTION MODEL OF ORBITAL TETHER SYSTEMS BASED ON PROPERTIES OF LIMIT CYCLES/ Valeriya Vorontsova, Olga Druzhinina//Nonlinearity: Problems, Solutions and Applications. Nova Science Publishers. New York.

Аннотация

The investigations of the influence of aerodynamics on the motion of an artificial two solid satellite-link are conditioned by the expansion of their field of application to orbital large extension tether systems. Aerodynamic effects are quite significant for such large space systems. The paper considers the classification of cylindrical phase space limit cycles and also researches the form of the limit cycle for the equation of the relative motion of two bodies orbital link with the influence of the gravitational effect, aerodynamic pressure, aero-gradient and dissipative factors, depending on the eccentricity growth and aerodynamic parameter. We use the associated motion equations taking into account gravity gradient and aerodynamic factors. An assessment of the influence of eccentricity and aerodynamic parameter changes on the behavior of limit cycles is also given in the paper. The research applies well-known methods of nonlinear mechanics: Lagrange equations of the first kind.

Ключевые слова

dynamics of space systems, orbital bunch of bodies, tether systems, qualitative theory of dynamical systems, limit cycles, cylindrical phase space, aerodynamic parameter, orbit eccentricity.

URL

https://www.novapublishers.com/catalog/product_info.php?products_id=62045&osCsid=0708c86070dcc8d55e6a8f72040d3653

Пожалуйста, используйте этот идентификатор, чтобы цитировать или ссылаться на эту карточку

https://repository.kpfu.ru/?p_id=160497

Полная запись метаданных

Поле DC	Значение	Язык
dc.contributor.author	Воронцова Валерия Леонидовна	ru_RU
dc.contributor.author	Druzhinina Olga Valentinovna	ru_RU
dc.date.accessioned	2017-01-01T00:00:00Z	ru_RU
dc.date.available	2017-01-01T00:00:00Z	ru_RU
dc.date.issued	2017	ru_RU
dc.identifier.citation	Valeriya Vorontsova. ANALYSIS OF A MOTION MODEL OF ORBITAL TETHER SYSTEMS BASED ON PROPERTIES OF LIMIT CYCLES/ Valeriya Vorontsova, Olga Druzhinina//Nonlinearity: Problems, Solutions and Applications. Nova Science Publishers. New York.	ru_RU
dc.identifier.uri	https://repository.kpfu.ru/?p_id=160497	ru_RU
dc.description.abstract	The investigations of the influence of aerodynamics on the motion of an artificial two solid satellite-link are conditioned by the expansion of their field of application to orbital large extension tether systems. Aerodynamic effects are quite significant for such large space systems. The paper considers the classification of cylindrical phase space limit cycles and also researches the form of the limit cycle for the equation of the relative motion of two bodies orbital link with the influence of the gravitational effect, aerodynamic pressure, aero-gradient and dissipative factors, depending on the eccentricity growth and aerodynamic parameter. We use the associated motion equations taking into account gravity gradient and aerodynamic factors. An assessment of the influence of eccentricity and aerodynamic parameter changes on the behavior of limit cycles is also given in the paper. The research applies well-known methods of nonlinear mechanics: Lagrange equations of the first kind.	ru_RU
dc.language.iso	ru	ru_RU
dc.subject	dynamics of space systems	ru_RU
dc.subject	orbital bunch of bodies	ru_RU
dc.subject	tether systems	ru_RU
dc.subject	qualitative theory of dynamical systems	ru_RU
dc.subject	limit cycles	ru_RU
dc.subject	cylindrical phase space	ru_RU
dc.subject	aerodynamic parameter	ru_RU
dc.subject	orbit eccentricity.	ru_RU
dc.title	ANALYSIS OF A MOTION MODEL OF ORBITAL TETHER SYSTEMS BASED ON PROPERTIES OF LIMIT CYCLES	ru_RU
dc.type	Зарубежные монографии	ru_RU