orientation

Analytical Solution of Differential Equations of Circular Spacecraft Orbit Orientation

Authors: Pankratov I. A., Chelnokov Y. N.

The problem of optimal reorientation of spacecraft’s orbit with a limited control, orthogonal to the plane of spacecraft orbit is being investigated. We have found an analytical solution of differential equations of circular spacecraft orbit orientation by control that is permanent on adjacent parts of the active spacecraft’s motion.

Analytical Solution of Equations of Near-circular Spacecraft’s Orbit Orientation

Authors: Pankratov I. A.

The problem of optimal reorientation of spacecraft’s orbit with a limited control, orthogonal to the plane of spacecraft’s orbit, is considered. An approximate analytical solution of differential equations of near-circular spacecraft’s orbit orientation by control, that is permanent on adjacent parts of the active spacecraft’s motion, is obtained.