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Six-Degree-of-Freedom Test FacilityShuttle to Space Station docking has become an important issue in the last few years. Docking sensors have been proposed that will provide the high precision measurements required for the fuel efficient rendezvous and docking of space vehicles. These sensors also will be used for satellite servicing and orbital assembly. The performance of the docking sensors must be tested before they are implemented in a space environment. A 6-DOF test facility was developed at the Tracking and Communications Section, JSC, to test the static and dynamic accuracies of docking sensors. A candidate sensor is evaluated by comparing the sensor's static position and velocity measurements to the more accurate 6-DOF system.
Document ID
19930012254
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bittel, Michelle A.
(Lockheed Engineering and Sciences Co. Houston, TX, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA, Washington, NASA Automated Rendezvous and Capture Review. Executive Summary
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N21443
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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