About the control and correction of exoatmospheric orbit-descent trajectory area for planet artificial satellite
Автор: Burdayev Mikhail Nikolayevich
Журнал: Программные системы: теория и приложения @programmnye-sistemy
Рубрика: Информационные системы в медицине
Статья в выпуске: 2 (20) т.5, 2014 года.
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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. \emph(in Russian).
Angle of entry into an atmosphere, descent, exoatmospheric trajectory area
Короткий адрес: https://sciup.org/14335977
IDR: 14335977
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