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A motion-constraint logic for moving-base simulators based on variable filter parametersA motion-constraint logic for moving-base simulators has been developed that is a modification to the linear second-order filters generally employed in conventional constraints. In the modified constraint logic, the filter parameters are not constant but vary with the instantaneous motion-base position to increase the constraint as the system approaches the positional limits. With the modified constraint logic, accelerations larger than originally expected are limited while conventional linear filters would result in automatic shutdown of the motion base. In addition, the modified washout logic has frequency-response characteristics that are an improvement over conventional linear filters with braking for low-frequency pilot inputs. During simulated landing approaches of an externally blown flap short take-off and landing (STOL) transport using decoupled longitudinal controls, the pilots were unable to detect much difference between the modified constraint logic and the logic based on linear filters with braking.
Document ID
19750003861
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Miller, G. K., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TN-D-7777
L-9585
Report Number: NASA-TN-D-7777
Report Number: L-9585
Accession Number
75N11933
Funding Number(s)
PROJECT: RTOP 504-29-14-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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