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 J Aerospace Sciences v 27 n 9 Sept 1960 p 653-8, 674)
Terminal guidance for rendezvous in space
Astronautical Sciences Rev
Astronautical Sciences Review ; 1 , n 4
1959
2 pages
Aufsatz (Zeitschrift)
Englisch
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