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. |