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Shuttle navigation overviewSpace Shuttle onboard navigation system tasks are related to position and velocity determination, attitude determination, sensor management, sensor Redundancy Management (RM), and navigation-related functions such as transformations, timing system utilization, and user processing for displays, guidance, and flight control. It is pointed out that Shuttle navigation is different in at least two areas from previous manned space flight navigation. The differences are related to the use of multiple units to provide protection from increased risk of failure of off-the-shelf-type equipment used for more than one flight, and the need to land at a runway. Attention is given to the navigation sensor system, the Shuttle Inertial Measurement Units, the Shuttle Star Tracker, the Crew Optical Alinement Sight, the Shuttle Tacan, the Air Data Subsystem, and aspects of navigation system mechanization.
Document ID
19820055465
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Savely, R. T.
(Rockwell International Corp. Downey, CA, United States)
Cockrell, B. F.
(NASA Johnson Space Center Houston, TX, United States)
Presser, P.
(Rockwell International Corp. Downey, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 82-1558
Report Number: AIAA PAPER 82-1558
Meeting Information
Meeting: Guidance and Control Conference
Location: San Diego, CA
Start Date: August 9, 1982
End Date: August 11, 1982
Accession Number
82A39000
Distribution Limits
Public
Copyright
Other

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