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High-precision buffer circuit for suppression of regenerative oscillationPrecision analog signal conditioning electronics have been developed for wind tunnel model attitude inertial sensors. This application requires low-noise, stable, microvolt-level DC performance and a high-precision buffered output. Capacitive loading of the operational amplifier output stages due to the wind tunnel analog signal distribution facilities caused regenerative oscillation and consequent rectification bias errors. Oscillation suppression techniques commonly used in audio applications were inadequate to maintain the performance requirements for the measurement of attitude for wind tunnel models. Feedback control theory is applied to develop a suppression technique based on a known compensation (snubber) circuit, which provides superior oscillation suppression with high output isolation and preserves the low-noise low-offset performance of the signal conditioning electronics. A practical design technique is developed to select the parameters for the compensation circuit to suppress regenerative oscillation occurring when typical shielded cable loads are driven.
Document ID
19950020839
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Tripp, John S.
(NASA Langley Research Center Hampton, VA, United States)
Hare, David A.
(NASA Langley Research Center Hampton, VA, United States)
Tcheng, Ping
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-4658
NAS 1.15:4658
L-17453
Report Number: NASA-TM-4658
Report Number: NAS 1.15:4658
Report Number: L-17453
Accession Number
95N27259
Funding Number(s)
PROJECT: RTOP 505-59-54-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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