Apollo lunar-descent guidance transfers the Lunar Module from a near-circular orbit to touchdown, traversing a 17 deg central angle and a 15 km altitude in 11 min. A group of interactive programs in an onboard computer guide the descent, controlling altitude and the descent propulsion system throttle. A ground-based program pre-computes guidance targets. The concepts involved in this guidance are described. Explicit and implicit guidance are discussed, guidance equations are derived, and the earlier Apollo explicit equation is shown to be an inferior special case of the later implicit equation. Interactive guidance, by which the two-man crew selects a landing site in favorable terrain and directs the trajectory there, is discussed. Interactive terminal-descent guidance enables the crew to control the essentially vertical descent rate in order to land in minimum time with safe contact speed. The altitude maneuver routine uses concepts that make gimbal lock inherently impossible.
Apollo lunar descent guidance
Automatica ; 10
1974-03-01
Sonstige
Keine Angabe
Englisch
Apollo LM Guidance Computer Software for the Final Lunar Descent
Tema Archiv | 1973
|Apollo lunar ascent and descent.
NTRS | 1967
|Apollo lunar descent and ascent trajectories
NTRS | 1970
|APOLLO Lunar Descent and Ascent Trajectories
NTIS | 1970
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