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Volumn 1, Issue , 1998, Pages 189-201
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Experimental study of active vibration suppression of flexible structure using modular control patch
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Author keywords
[No Author keywords available]
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Indexed keywords
DIGITAL SIGNAL PROCESSORS;
FIGHTER AIRCRAFT;
FLEXIBLE STRUCTURES;
PIEZOELECTRIC CERAMICS;
SIGNAL PROCESSING;
STRAIN RATE;
ACTUATORS;
ALGORITHMS;
CERAMIC MATERIALS;
DIGITAL CONTROL SYSTEMS;
DIGITAL SIGNAL PROCESSING;
FEEDBACK CONTROL;
PIEZOELECTRIC TRANSDUCERS;
POSITION CONTROL;
SENSORS;
VIBRATION CONTROL;
ACTIVE VIBRATION SUPPRESSION;
DIGITAL CONTROLLERS;
MULTI-MODE VIBRATIONS;
PIEZOCERAMIC SENSORS;
POSITIVE POSITION FEEDBACK;
STRAIN RATE FEEDBACK;
UNITED STATES AIR FORCE;
VIBRATION SUPPRESSION;
FEEDBACK;
SPACECRAFT;
ACTIVE VIBRATION SUPPRESSION;
MODULAR CONTROL PATCH (MCP);
POSITIVE POSITION FEEDBACK (PPF) CONTROL;
STRAIN RATE FEEDBACK (SRF) CONTROL;
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EID: 0031629554
PISSN: 1095323X
EISSN: None
Source Type: Conference Proceeding
DOI: 10.1109/AERO.1998.686818 Document Type: Conference Paper |
Times cited : (32)
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References (7)
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