Article examines several problems related to control of interplanetary missile; equations of motion about center of mass, and conclusions from law of conservation of angular momentum; example of application of derived equations to case of small deflections of missile from given attitude. (English translation from Russian version of Artificial Earth Satellites n 5 1960 p 41-53)
Some guidance problems in interplanetary space
ARS J
ARS Journal ; 31 , n 11
1961
7 pages
Article (Journal)
English
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