NASA NTRS · 19680056621
Computer-aided inertial platform realignment in manned space flight.
Abstract
Hardware design and functions of Apollo guidance and navigation system for inertial measurement unit realignment, outlining computer programs and routines
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Hand, J. A.. 1968-08-01. Computer-aided inertial platform realignment in manned space flight.. https://ntrs.nasa.gov/citations/19680056621
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