Full Article: PDF
Digital Object Identifier System: http://dx.doi.org/10.15863/TAS.2014.06.14.1
Language: Russian
Citation: Chernyshov AD, Gorjajnov VV, Chernyshov OA (2014) CALCULATION OF FLIGHT OF A SPACECRAFT ON THE EXOATMOSPHERIC PORTION OF THE TRAJECTORY BY THE METHOD RAPID EXPANSIONS. ISJ Theoretical & Applied Science 06 (14): 1-4. doi: http://dx.doi.org/10.15863/TAS.2014.06.14.1 |
Pages: 1-4
Published: 30.06.2014
Abstract: The problem of the motion of a spacecraft on the exoatmospheric portion of the trajectory. An analytical solution by rapid expansions. Shows the absolute error of the trajectory of a spacecraft, its speed and acceleration, which showed high efficiency of the method rapid expansions.
Key words: Spacecraft, flight trajectory, rapid expansion, an analytical solution.
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