Design requirements for the Flight Control System of America’s first manned lunar landing vehicle are discussed in terms of broad mission aspects.Basic functions of the combined control-guidance-propulsion loop are discussed in relation to mission sequence of events.Two critical design areas, reliability and the man/machine interface, are discussed in detail and some design approaches are reviewed.
LEM FLIGHT CONTROL - A STATEMENT OF THE PROBLEM
Sae Technical Papers
SAE World Congress & Exhibition ; 1964
1964-01-01
Conference paper
English
LEM flight control -- Statement of problem
Engineering Index Backfile | 1964
|Springer Verlag | 2020
|Propulsive-Only Flight Control Problem
NTIS | 1996
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