Finite-thrust explicit guidance law for nearly circular orbital rendezvous.
ZEE, C.-H. /GRUMMAN AIRCRAFT ENGINEERING CORP., GUIDANCE AND CONTROLSECTION, TRAJECTORY ANALYSIS GRO
JOURNAL OF SPACECRAFT AND ROCKETS ; 4 , 1 ; 34-38
1967
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Finite-thrust explicit guidance law for nearly circular orbital rendezvous
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