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Program Systems: Theory and Applications, 2013, Volume 4, Issue 4, Pages 3–15
(Mi ps97)
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This article is cited in 3 scientific papers (total in 3 papers)
Optimization Methods and Control Theory
The repositioning maneuver of artificial Earth satellite in a circular orbit with a supporting acceleration
M. N. Burdayev Yu. A. Gagarin State Scientific Research and Testing Cosmonaut Training Center
Abstract:
The paper reveals the maneuver entity of reposition artificial satellite on a circular orbit with a supporting acceleration. A maneuver program implementation with using of constant thrust motors is found and proved. An energy efficiency of maneuver under various conditions of its implementation is determined. (in Russian)
Key words and phrases:
maneuver, satellite, circular orbit, supporting acceleration, trajectory.
Citation:
M. N. Burdayev, “The repositioning maneuver of artificial Earth satellite in a circular orbit with a supporting acceleration”, Program Systems: Theory and Applications, 4:4 (2013), 3–15
Linking options:
https://www.mathnet.ru/eng/ps97 https://www.mathnet.ru/eng/ps/v4/i4/p3
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Statistics & downloads: |
Abstract page: | 157 | Full-text PDF : | 62 | References: | 36 | First page: | 1 |
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