NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Discrete distributed strain sensing of intelligent structuresTechniques are developed for the design of discrete highly distributed sensor systems for use in intelligent structures. First the functional requirements for such a system are presented. Discrete spatially averaging strain sensors are then identified as satisfying the functional requirements. A variety of spatial weightings for spatially averaging sensors are examined, and their wave number characteristics are determined. Preferable spatial weightings are identified. Several numerical integration rules used to integrate such sensors in order to determine the global deflection of the structure are discussed. A numerical simulation is conducted using point and rectangular sensors mounted on a cantilevered beam under static loading. Gage factor and sensor position uncertainties are incorporated to assess the absolute error and standard deviation of the error in the estimated tip displacement found by numerically integrating the sensor outputs. An experiment is carried out using a statically loaded cantilevered beam with five point sensors. It is found that in most cases the actual experimental error is within one standard deviation of the absolute error as found in the numerical simulation.
Document ID
19930047263
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, Mark S.
(NASA Headquarters Washington, DC United States)
Crawley, Edward F.
(MIT Cambridge, MA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: Joint Japan(U.S. Conference on Adaptive Structures, 2nd, Nagoya, Japan, Nov. 12-14, 1991, Collection of Papers (A93-31226 11-18)
Publisher: Technomic Publishing Co., Inc.
Subject Category
Instrumentation And Photography
Accession Number
93A31260
Funding Number(s)
CONTRACT_GRANT: NAGW-1335
CONTRACT_GRANT: F49620-92-J-0010
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available