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Adaptive position control loopDesign of attitude control system for a sounding rocket is established by using a control loop which incorporates a lead network to convert position output into a feedback signal that is approximately proportional to position, plus a constant times rate.
Document ID
19720000052
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Keltz, W. L. (GE)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Electronic Systems
Report/Patent Number
ARC-10255
Report Number: ARC-10255
Accession Number
72B10052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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