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
Yu. G. Sikharulidze, A. S. Karpov, R. K. IvanovVolume:
43
Language:
english
Pages:
19
DOI:
10.1007/s10604-005-0055-z
Date:
September, 2005
File:
PDF, 166 KB
english, 2005