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The Shuttle inertial systemThe Space Shuttle inertial system is built around a sensor assembly called the inertial measurement unit (IMU). The system includes a redundant set of three structurally integrated IMU's that operate in conjunction with parallel strung data system computers to provide precise attitude and velocity information to user system functions. The inertial system is actually a separate subsystem function integrated into the overall avionics system. Software resident in the system computers is the final link in the inertial system. The inertial software is comprised of two major sets, including a subsystem operating program (SOP) called the IMU SOP and redundancy management. Attention is given to system applications, systems performance, attitude sensitivities, the IMU platform, IMU thermal management, aspects of IMU calibration, and Shuttle program experience.
Document ID
19820055427
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Swingle, W. L.
(NASA Johnson Space Center Avionics Systems Div., Houston, TX, United States)
Kang, Y.
(Rockwell International Corp. Downey, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 82-1559
Meeting Information
Meeting: Guidance and Control Conference
Location: San Diego, CA
Start Date: August 9, 1982
End Date: August 11, 1982
Accession Number
82A38962
Distribution Limits
Public
Copyright
Other

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