Low thrust spacecraft motion control with simultaneous changes in main orbital elements

  • Pavel Fadeenkov
  • Sergey Ishkov

Abstract

The problem of forming a nominal optimal program for controlling the direction of the low-thrust vector of a spacecraft for a significant change in the elements of the spatial orbit is considered. A scheme for the joint change of the elements of the orbit within the framework of a simple structure for controlling the thrust vector on the orbit is proposed.

Published
2019-11-20