DocumentCode :
1305387
Title :
NASA´s Anderson Loop
Author :
Anderson, Karl F.
Volume :
1
Issue :
1
fYear :
1998
fDate :
3/1/1998 12:00:00 AM
Firstpage :
5
Abstract :
The Anderson loop is a simply implemented measurement circuit topology that uses active subtraction instead of the passive subtraction accomplished by the classic Wheatstone bridge. Larger, inherently linear signals from sensing-element impedance change are available with less excitation power and without the use of transmitters to achieve immunity to wire-resistance variations. Transducers can be designed with any convenient quantity of sensor elements. Transducer intelligence can be implemented within the signal conditioner. The change in a single sensing element can be used in several simultaneous measurements. Sensor elements can appear to have any desired impedance level and influence on any of several outputs
Keywords :
aerospace test facilities; signal processing equipment; Anderson Loop; NASA; Wheatstone bridge; active subtraction; dual differential subtraction; impedance level; linear signals; measurement circuit topology; sensing-element impedance; signal conditioner; simultaneous measurements; transducer intelligence; Bridge circuits; Circuit topology; Impedance; Intelligent sensors; Transducers; Transmitters;
fLanguage :
English
Journal_Title :
Instrumentation & Measurement Magazine, IEEE
Publisher :
ieee
ISSN :
1094-6969
Type :
jour
DOI :
10.1109/5289.658270
Filename :
658270
Link To Document :
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