Planar relative motion between target and interceptor satellite is treated by perturbation techniques to obtain linearized equations of motion which are valid in vicinity of collision course; terminal guidance law is formulated for attaining collision course and for achievement of satellite rendezvous using constant thrust rocket motors.
Terminal guidance technique for satellite interception utilizing constant thrust rocket motor
ARS -- J
ARS Journal ; 30 , n 9
1960
2 pages
Article (Journal)
English
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