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Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II
- Authors: Salmin V.V.1, Vassiliev V.V.1, Ishkov S.A.1, Romanenko V.A.1, Sokolov V.O.1, Starinova O.L.1, Yurin V.V.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 7, No 1 (2008)
- Pages: 45-67
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/544
- DOI: https://doi.org/10.18287/2541-7533-2008-0-1(14)-45-67
- ID: 544
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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
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