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NASA MSFC hardware in the loop simulations of automatic rendezvous and capture systemsTwo complementary hardware-in-the-loop simulation facilities for automatic rendezvous and capture systems at MSFC are described. One, the Flight Robotics Laboratory, uses an 8 DOF overhead manipulator with a work volume of 160 by 40 by 23 feet to evaluate automatic rendezvous algorithms and range/rate sensing systems. The other, the Space Station/Station Operations Mechanism Test Bed, uses a 6 DOF hydraulic table to perform docking and berthing dynamics simulations.
Document ID
19930012259
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tobbe, Patrick A.
(Logicon Control Dynamics Co. Huntsville, AL., United States)
Naumann, Charles B.
(Logicon Control Dynamics Co. Huntsville, AL., United States)
Sutton, William
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Bryan, Thomas C.
(NASA Marshall Space Flight Center Huntsville, AL, 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
93N21448
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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