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Seminar of Control System Department
February 20, 2014, Ekaterinburg, ul. S Kovalevskoi, 16, room 322
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The problem of optimal injection of a launcher into a circumglobal orbit
V. B. Kostousov, I. N. Kandoba, A. B. Lozhnikov |
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Abstract:
The control problems connected with the injection of a carrier rocket (launcher) into a given circumglobal elliptic orbit are considered. The motion of the launcher is described by a nonlinear dynamic system. In some important practical problems, there are some additional requirements on a desired control. One of them consists in the maximization of a payload mass led to the orbit.
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