A Concept of Guidance for an Air-Launch Vehicle with Compensation of Initial Downrange and Launch Time Errors at Direct Insertion into a Rendezvous Point in the Orbit

Author： Sikharulidze Yu.   Karpov A.   Ivanov R.  

Publisher： MAIK Nauka/Interperiodica

ISSN： 0010-9525

Source： Cosmic Research, Vol.43, Iss.5, 2005-09, pp. : 342-360

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