Review of satellite rendezvous terminal guidance requirements; command guidance system is envisioned for space station application with position information being obtained by pulse radar, digital computer, infrared horizon scanner, and command link; rendezvous problem associated with satellite inspection; terminal guidance system would be composed of radar, digital computer and propulsion system. (See also Astronautical Sciences Rev v 1 n 4 Oct-Dec 1959 p 9-10)
Terminal guidance for rendezvous in space
J Aerospace Sciences
Journal of Aerospace Science ; 27 , n 9
1960
Aufsatz (Zeitschrift)
Englisch
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