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.
Hardware Specific Integration Strategy for Impedance-Based Structural Health Monitoring of Aerospace Systems
2011
26 pages
Report
Keine Angabe
Englisch
Space Launch Vehicles & Support Equipment , Resistive, Capacitive, & Inductive Components , Detection & Countermeasures , Aerospace systems , Systems health monitoring , Systems integration , Hardware , Aircraft structures , Electrical impedance , Nondestructive tests , Feasibility analysis , Prototypes , Systems engineering , Flight tests , Wings , Piezoelectricity
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