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FACE computer simulationA computer simulation of the FACE (Flexible Arm Controls Experiment) was conducted to assess its design for use in the Space Shuttle. The FACE is supposed to be a 14-ft long articulate structure with 4 degrees of freedom, consisting of shoulder pitch and yaw, elbow pitch, and wrist pitch. Kinematics of the FACE was simulated to obtain data on arm operation, function, workspace and interaction. Payload capture ability was modeled. The simulation indicates the capability for detailed kinematic simulation and payload capture ability analysis, and the feasibility of real-time simulation was determined. In addition, the potential for interactive real-time training through integration of the simulation with various interface controllers was revealed. At this stage, the flexibility of the arm was not yet considered.
Document ID
19910042192
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sadeh, Willy Z.
(Colorado State University Fort Collins, United States)
Szmyd, Jeffrey A.
(Lockheed Engineering and Sciences Co. Houston, TX, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 90-037
Meeting Information
Meeting: Annual Rocky Mountain Guidance and Control Conference
Location: Keystone, CO
Country: United States
Start Date: February 3, 1990
End Date: February 7, 1990
Sponsors: AAS
Accession Number
91A26815
Distribution Limits
Public
Copyright
Other

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