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Mitigating Motion Base Safety Issues: The NASA LaRC CMF ImplementationThe NASA Langley Research Center (LaRC), Cockpit Motion Facility (CMF) motion base design has taken advantage of inherent hydraulic characteristics to implement safety features using hardware solutions only. Motion system safety has always been a concern and its implementation is addressed differently by each organization. Some approaches rely heavily on software safety features. Software which performs safety functions is subject to more scrutiny making its approval, modification, and development time consuming and expensive. The NASA LaRC's CMF motion system is used for research and, as such, requires that the software be updated or modified frequently. The CMF's customers need the ability to update the simulation software frequently without the associated cost incurred with safety critical software. This paper describes the CMF engineering team's approach to achieving motion base safety by designing and implementing all safety features in hardware, resulting in applications software (including motion cueing and actuator dynamic control) being completely independent of the safety devices. This allows the CMF safety systems to remain intact and unaffected by frequent research system modifications.
Document ID
20050232875
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Bryant, Richard B., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Grupton, Lawrence E.
(NASA Langley Research Center Hampton, VA, United States)
Martinez, Debbie
(NASA Langley Research Center Hampton, VA, United States)
Carrelli, David J.
(Swales Aerospace Hampton, VA, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2005
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA Paper 2005-6107
Meeting Information
Meeting: AIAA Modeling and Simulation Technologies Conference and Exhibit
Location: San Francisco, CA
Country: United States
Start Date: August 15, 2005
End Date: August 18, 2005
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 23-090-70-10
Distribution Limits
Public
Copyright
Public Use Permitted.
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