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Program Systems: Theory and Applications, 2014, Volume 5, Issue 2, Pages 13–18
(Mi ps116)
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Optimization Methods and Control Theory
About the control and correction of exoatmospheric orbit-descent trajectory area for planet artificial satellite
M. N. Burdayev The Yuri Gagarin Russian State Science Research Cosmonauts Training Centre
Abstract:
The article shows the results of applying cognitive graphics method to calculating problem approximate solution of exoatmospheric orbit-descent trajectory area parameters for planets artificial satellites. Presented graphically form for this problem general solution on the example of descent into Earth’s atmosphere. (in Russian).
Key words and phrases:
descent, exoatmospheric trajectory area, angle of entry into an atmosphere.
Citation:
M. N. Burdayev, “About the control and correction of exoatmospheric orbit-descent trajectory area for planet artificial satellite”, Program Systems: Theory and Applications, 5:2 (2014), 13–18
Linking options:
https://www.mathnet.ru/eng/ps116 https://www.mathnet.ru/eng/ps/v5/i2/p13
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| Statistics & downloads: |
| Abstract page: | 328 | | Full-text PDF : | 223 | | References: | 62 |
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