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Program Systems: Theory and Applications, 2014, Volume 5, Issue 2, Pages 13–18 (Mi ps116)  

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
References:
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.
Document Type: Article
UDC: 629.7.05
Language: Russian
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
Citation in format AMSBIB
\Bibitem{Bur14}
\by M.~N.~Burdayev
\paper About the control and correction of exoatmospheric orbit-descent trajectory area for planet artificial satellite
\jour Program Systems: Theory and Applications
\yr 2014
\vol 5
\issue 2
\pages 13--18
\mathnet{http://mi.mathnet.ru/ps116}
Linking options:
  • https://www.mathnet.ru/eng/ps116
  • https://www.mathnet.ru/eng/ps/v5/i2/p13
  • Citing articles in Google Scholar: Russian citations, English citations
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    Program Systems: Theory and Applications
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