Article

Cover

Title

Problem optimum spaceship trajectory to inspect or service system of body

Author

V.S. Korolev

Organization

Saint-Petersburg State University
Saint-Petersburg, Russia

Abstract

Optimum trajectories of transitions of spacecrafts between various orbits of space objects are considered. It is required to define a set of admissible decisions taking into account possible restrictions on time and energy expenses. It is necessary to satisfy consistently these conditions for all objects from the marked-out set.

Keywords

celestial mechanics, mathematical models, optimal solutions

For citing this article

Korolev V.S. Problem optimum spaceship trajectory to inspect or service system of body // The Research of the Science City, 2015, no. 2, pp. 18-23.

This Article is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).