1.Principles of operation

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2.The hardware components of the LM NGC System

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Figure 2.1 Detailed systems diagram of the Apollo LM Navigation, Guidance and Control System
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Figure 2.2
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Figure 2.3
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3.Flight Control Modes

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4.Title

Acronyms

ACA Attitude Controller Assembly AEA Abort Electronics Assembly AEAA Ascent Engine Arming Assembly AGS Abort Guidance System AOT Alignment Optical Telescope APS Ascent Propulsion System ASA Abort Sensor Assembly ATCA Attitude and Translation Control Assembly CDU Coupling Data Unit CES Control Electronics System DECA Descent Engine Control Assembly DEDA Data Entry and Display Assembly DPS Descent Propulsion System DSKY Display and Keyboard

FDAI Flight Director Attitude Indicator GASTA Gimbal Angle Sequencing Transformation Assembly GDA Gimbal Drive Actuator IMU Inertial Measurement Unit LGC Lunar Module Guidance Computer LM Lunar Module PGNCS Primary Guidance, Navigation & Control System PTA Pulse Torque Assembly RCS Reaction Control System RGA Rate Gyro Assembly TTCA Thrust/Translation Controller Assembly

References LM/AGS Operating Manual Flight Program 6 TRW Report 11176-6033-T000, Rev.1, April 1969 by R.L. Mendelsberg for NASA, Manned Spacecraft Center, Houston, Texas Ref. Ref. Ref. Ref.

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