About control possibility of a satellite attitude


Zaure B.Rakisheva;


<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


About control possibility of a satellite attitude;very;


To explore the background and basis of the node document

Springer Journals Database

Total: 0 articles

Similar documents

Documents that have the similar content to the node document