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A g-load display for remotely piloted vehicles and other aircraft that are subject to maneuvering constraintsThe absence of kinesthetic cues deprives RPV pilots of essential feedback, particularly during high speed maneuvers. A display was designed to facilitate pilot control of g loads and to permit an immediate indication of g-load constraint violations. The display embodies all the motion vector components that contribute to maneuvering accelerations. In one mode of operation, the device displays the components of angular velocity as variable length pointers emanating from the center of a circle whose radius is determined by the linear velocity of the vehicle. An alternative mode of operation permits the pilot to select a display in which g loads are presented directly as variable length pointers emanating from the center of a circle whose radius is again determined by the linear velocity of the vehicle. Each circle defines a safe region of operation, and penetration of the circumference of the appropriate circle by a pointer implies that the structural design load was exceeded.
Document ID
19750022085
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Howard, J. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Aircraft Instrumentation
Report/Patent Number
A-6032
NASA-TN-D-8056
Report Number: A-6032
Report Number: NASA-TN-D-8056
Accession Number
75N30158
Funding Number(s)
PROJECT: RTOP 504-09-33-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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