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Space Navigation Guidance and Control, Volume 1

Space Navigation Guidance and Control, Volume 2

Study of powered descent trajectories for manned lunar landings, Project Apollo, August 9, 1963

NASA TM X-58040 Apollo Lunar Decent and Ascent Trajectories (ALSJ)

Apollo CSM and LM onboard navigation system constraints

Apollo: Guidance and control system

Apollo: Guidance and control system 2

NASA TND 6846 Apollo Experience Report-Mission Planning for Lunar Module Decent and Ascent pages 1-18 (ALSJ)

NASA TND 6846 Apollo Experience Report-Mission Planning for Lunar Module Decent and Ascent pages 19-42(ALSJ)

APOLLO LUNAR-DESCENT GUIDANCE

A LM powered descent strategy

Possible Simplification of the Apollo Entry Guidance

LM powered descent trajectory for the Apollo lunar landing mission

LM Descent Guidance for a Feasibility Study to Simplify Apollo Guidance

LM powered ascent trajectory for the Apollo lunar landing mission

Project Apollo - A proposed LEM descent trajectory and fuel budget

Simplified Software for the Apollo Guidance Computer - CSM Powered Flight Programs

Apollo mission techniques. Mission C-prime lunar (alternate 1) translunar midcourse corrections and lunar orbit insertion. Volume 1: Techniques description, revision A

Preliminary analysis of LM abort and CSM rescue from 60-n. mi. CSM orbit during the Hohmann descent phase

Analysis of current LEM powered-descent trajectories

Project Apollo. A preliminary simulation study of the required velocity meter sensitivity and touchdown control performance during lunar landing

Apollo guidance and navigation. Volume 2 Primary G and N system lunar orbit operations

Description of Apollo Entry Guidance

MIT's role in Project Apollo. Volume 3: Computer subsystem

MIT's role in Project Apollo. Volume 5: The software effort

Apollo Lunar-Descent Guidance

Reliability history of the Apollo guidance computer

Lunar descent and ascent trajectories

Delta V performance of the Apollo LM ascent trajectory

Dynamic analysis of the LEM flight control system

Apollo guidance and navigation. Guidance and navigation system for lunar excursion module (1962)

Preliminary analysis of LM abort and CSM rescue from a 60-n mi. circular orbit following an LM abort from powered descent

Manual abort guidance from the midcourse region of a lunar mission

A linearized error analysis of onboard primary navigation systems for the Apollo lunar module

A simplified guidance scheme for aborting lunar landings

Analysis of sextant navigation measurements during lunar module rendezvous

A simple abort scheme for lunar landings

Revised LM descent and ascent delta V budgets for the lunar landing mission

A method for star vector determination from alignment optical telescope sighting

Real-time data processing and orbit determination on the Apollo tracking ships

Apollo navigation ground and onboard capabilities

Summary of Apollo guidance and navigation error analysis

Maximum allowable lateral velocity errors during LM powered descent - Program Apollo

Apollo Primary Guidance Navigation and Control System, addendum PGNCS Final report