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A solution of the optimal turn problem of an axially symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions
A. V. Molodenkov, Ya. G. SapunkovVolume:
46
Language:
english
Pages:
14
DOI:
10.1134/s1064230707020189
Date:
April, 2007
File:
PDF, 301 KB
english, 2007