Presentations and control requirements for manned astrovehicle employed for interception of artificial satellites during terminal phase of orbital rendezvous; two oscilloscope and one direct visual observation presentation and three control modes were investigated; study is considered in terms of manned interceptor having home berth at manned space station in circular orbit 500 mi above earth.
Simulator investigation of controls and display required for terminal phase of coplanar orbital rendezvous
NASA -- Tech Note
1960
30 pages
Article (Journal)
English
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Engineering Index Backfile | 1959
|Terminal spacecraft coplanar rendezvous control
AIAA | 1995
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Online Contents | 1995
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