The avionics subsystem of the Common Lunar Lander (CLL) is designed to meet the following requirements: guidance, navigation, and control of the spacecraft; central computer for all subsystems; and data storage for all subsystems for telemetry purposes. A table describing the av ionics subsystem is listed. Additionally, a schematic representation of the avionics subsystem is provided.
Avionics Subsystem
1991-09-17
Miscellaneous
No indication
English
NTIS | 1991
|Space avionics stellar-inertial subsystem
IEEE | 2001
|Space Avionics Stellar-Inertial Subsystem
British Library Conference Proceedings | 2001
|Advanced Spacesuit Avionics Subsystem Integration Testing
British Library Conference Proceedings | 2014
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