About control possibility of a satellite attitude

【Author】

Zaure B.Rakisheva;

【Abstract】

<正>As is known motion of a satellite relative to its center of mass may be considered as the rotational motion of a solid body with fixed point in gravitational field of forces.This motion is described by the system of nonlinear ordinary differential equations of Euler. In paper with a help of original linear change of variables the initial system is reduced to the normal type,i.e.,to the system

【Keywords】

About control possibility of a satellite attitude;very;

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