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    기술보고서 게시판 내용
    타이틀 Hardware Specific Integration Strategy for Impedance-Based Structural Health Monitoring of Aerospace Systems
    저자 Owen, Robert B.;; Gyekenyesi, Andrew L.;; Inman, Daniel J.;; Ha, Dong S.
    Keyword AEROSPACE SYSTEMS;; AIRCRAFT STRUCTURES;; ELECTRICAL IMPEDANCE;; FEASIBILITY ANALYSIS;; FLIGHT TESTS;; HARDWARE;; NONDESTRUCTIVE TESTS;; PIEZOELECTRICITY;; PROTOTYPES;; SYSTEMS ENGINEERING;; SYSTEMS HEALTH MONITORING;; SYSTEMS INTEGRATION;; WINGS
    URL http://hdl.handle.net/2060/20110012575
    보고서번호 NASA/CR-2011-217153
    발행년도 2011
    출처 NTRS (NASA Technical Report Server)
    ABSTRACT The Integrated Vehicle Health Management (IVHM) Project, sponsored by NASA''s Aeronautics Research Mission Directorate, is conducting research to advance the state of highly integrated and complex flight-critical health management technologies and systems. An effective IVHM system requires Structural Health Monitoring (SHM). The impedance method is one such SHM technique for detection and monitoring complex structures for damage. This position paper on the impedance method presents the current state of the art, future directions, applications and possible flight test demonstrations.

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