The development of validated multidisciplinary Integrated Vehicle Health Management (IVHM) tools, technologies, and techniques to enable detection, diagnosis, prognosis, and mitigation in the presence of adverse conditions during flight will provide effective solutions to deal with safety related challenges facing next generation aircraft. The adverse conditions include loss of control caused by environmental factors, actuator and sensor faults or failures, and damage conditions. A major concern in these structures is the growth of undetected damage (cracks) due to fatigue and low velocity foreign impacts that can reach a critical size during flight, resulting in loss of control of the aircraft. Hence, development of efficient methodologies to determine the presence, location, and severity of damage in critical structural components is highly important in developing efficient structural health management systems.
Damage Characterization Method for Structural Health Management Using Reduced Number of Sensor Inputs
13th AIAA Gossamer Systems Forum
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2012
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Honolulu, HI, United States
20th AIAA/ASME/AHS Adaptive Structures Conference
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2012
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Honolulu, HI, United States
14th AIAA Non-Deterministic Approaches Conference
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2012
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Honolulu, HI, United States
53rd Structures, Structural Dynamics, and Materials Conference (SDM)
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2012
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Honolulu, HI, United States
2012-04-18
Conference paper
No indication
English
British Library Conference Proceedings | 2012
|Damage Characterization Using the Extended Finite Element Method for Structural Health Management
British Library Conference Proceedings | 2011
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