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Multisensor Arrays for Greater Reliability and AccuracyArrays of multiple, nominally identical sensors with sensor-output-processing electronic hardware and software are being developed in order to obtain accuracy, reliability, and lifetime greater than those of single sensors. The conceptual basis of this development lies in the statistical behavior of multiple sensors and a multisensor-array (MSA) algorithm that exploits that behavior. In addition, advances in microelectromechanical systems (MEMS) and integrated circuits are exploited. A typical sensor unit according to this concept includes multiple MEMS sensors and sensor-readout circuitry fabricated together on a single chip and packaged compactly with a microprocessor that performs several functions, including execution of the MSA algorithm. In the MSA algorithm, the readings from all the sensors in an array at a given instant of time are compared and the reliability of each sensor is quantified. This comparison of readings and quantification of reliabilities involves the calculation of the ratio between every sensor reading and every other sensor reading, plus calculation of the sum of all such ratios. Then one output reading for the given instant of time is computed as a weighted average of the readings of all the sensors. In this computation, the weight for each sensor is the aforementioned value used to quantify its reliability. In an optional variant of the MSA algorithm that can be implemented easily, a running sum of the reliability value for each sensor at previous time steps as well as at the present time step is used as the weight of the sensor in calculating the weighted average at the present time step. In this variant, the weight of a sensor that continually fails gradually decreases, so that eventually, its influence over the output reading becomes minimal: In effect, the sensor system "learns" which sensors to trust and which not to trust. The MSA algorithm incorporates a criterion for deciding whether there remain enough sensor readings that approximate each other sufficiently closely to constitute a majority for the purpose of quantifying reliability. This criterion is, simply, that if there do not exist at least three sensors having weights greater than a prescribed minimum acceptable value, then the array as a whole is deemed to have failed.
Document ID
20110016813
Acquisition Source
Kennedy Space Center
Document Type
Other - NASA Tech Brief
Authors
Immer, Christopher
(DYNACS Engineering Co., Inc. Cocoa Beach, FL, United States)
Eckhoff, Anthony
(DYNACS Engineering Co., Inc. Cocoa Beach, FL, United States)
Lane, John
(DYNACS Engineering Co., Inc. Cocoa Beach, FL, United States)
Perotti, Jose
(DYNACS Engineering Co., Inc. Cocoa Beach, FL, United States)
Randazzo, John
(DYNACS Engineering Co., Inc. Cocoa Beach, FL, United States)
Blalock, Norman
(DYNACS Engineering Co., Inc. Cocoa Beach, FL, United States)
Ree, Jeff
(DYNACS Engineering Co., Inc. Cocoa Beach, FL, United States)
Date Acquired
August 25, 2013
Publication Date
July 1, 2004
Publication Information
Publication: NASA Tech Briefs, July 2004
Subject Category
Man/System Technology And Life Support
Report/Patent Number
KSC-12221/359
Distribution Limits
Public
Copyright
Public Use Permitted.
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