Function of midcourse guidance is to place intercepting vehicle in close proximity to satellite; 2-dimensional geometry and circular target orbits only are considered; equations are developed yielding required velocity corrections necessary for interception as function of rocket's present position and velocity, relative to target; numerical computation.
Midcourse guidance problem in satellite interception -- 1
ARS -- J
ARS Journal ; 30 , n 1
1960
6 pages
Article (Journal)
English
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