Dynamics of Rotational Motion of the Satellite in Sunlight Flux

Авторы: Beletsky V.V., Kuleshov A.S.
Сборник: Proceedings - Fifth EUROMECH Nonlinear Dynamics Conference: August 7-12, 2005, Eindhoven University of Technology
Год издания: 2005
Место издания: Technische Universiteit Eindhoven
Первая страница: 03-113
Последняя страница: 03-128
Аннотация: We consider the motion of an axially symmetric satellite about its center of mass under the solar radiation torques. The satellite has an axially symmetric solar stabilizer and a number of paddles arranged like a windmill. The total moment of forces may be represented as superposition of a conservative moment and a propelling torque. The equations in evolutionary variables are used to study the attitude dynamics. The averaged system of equations is obtained. This averaged system admits one first integral and an invariant measure, but in general case it is not integrable: for integrability we need another first integral. The phase space structure is investigated. The results of numerical simulations are represented as 2D graphs.
Добавил в систему: Кулешов Александр Сергеевич

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