Apollo experience report--guidance and control systems: primary guidance, navigation, and control system development
M. D. Holley, Lyndon B. Johnson Space Center, United States. National Aeronautics and Space Administration
National Aeronautics and Space Administration, 1976 - Science - 63 pages
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accelerometers alinement Apollo 16 Apollo guidance computer Apollo mission Apollo Program basic bearing beryllium Block I 100 Block I I capability capacitor caused circuits coldplate components COMPUTER SUBSYSTEM configuration connector contamination coupling data units damping fluid design change development contractor diode display DSKY ECDU electronics erasable memory evaluation eyepiece failure mode fixed memory flatpack flight functions G&N system gate gimbal gimbal lock hardware heater in-flight repair incorporated incrementing INERTIAL REFERENCE INTEGRATING inertial subsystem input instructions instruments integrated circuit interconnect IRIG Johnson Space Center limit-cycle located logic lunar magnetic major manufacturing mechanical metal mounted operation optical subsystem output package performance PGNCS PIPA Polaris Mark primary guidance problem PULSED INTEGRATING PENDULOUS REFERENCE INTEGRATING GYRO registers relays reliability repair program resistors resulted rope memory screen seal signal spacecraft switching techniques temperature test program tion torque transistor tray vibration wheel wire