Micro-rendezvous operation is defined as phase of orbital rendezvous which starts at relative range on order of 50-100,000 ft and terminates in docking operation; display of navigation data in forms of control criteria, which involve specification of thrust and vehicle attitude requirements, is introduced; control criteria requiring minimum of predisplay computation and resulting in simple cockpit displays are developed for orthogonal thrust vectors system, single vectored thrust system, and on-off system.
Control criteria for manual orbital rendezvous
Am Astronautical Soc -- Advances Astronautical Sciences
1963
25 pages
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1959
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