Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II

Abstract


The second part of the article presents the results of solving some applied problems of flights of space vehicles with low-thrust engines.


About the authors

V. V. Salmin

Samara State Aerospace University

Author for correspondence.
Email: sputnik@ssau.ru

Russian Federation

V. V. Vassiliev

Samara State Aerospace University

Email: sputnik@ssau.ru

Russian Federation

S. A. Ishkov

Samara State Aerospace University

Email: irkt@ssau.ru

Russian Federation

V. A. Romanenko

Samara State Aerospace University

Email: sputnik@ssau.ru

Russian Federation

V. O. Sokolov

Samara State Aerospace University

Email: sputnik@ssau.ru

Russian Federation

O. L. Starinova

Samara State Aerospace University

Email: starinova@ssau.ru

Russian Federation

V. V. Yurin

Samara State Aerospace University

Email: sputnik@ssau.ru

Russian Federation

References

Statistics

Views

Abstract - 38

PDF (Russian) - 21

Article Metrics

Metrics Loading ...

PlumX

Dimensions

Refbacks

  • There are currently no refbacks.

Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies