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Volumn 2, Issue , 2005, Pages 833-843
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Development and qualification of active vibration control system for the eurocopter EC225/EC725
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Author keywords
[No Author keywords available]
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Indexed keywords
ACTIVE ANTI-VIBRATION SYSTEM;
ACTIVE VIBRATION CONTROL SYSTEMS;
ANTI-VIBRATION DEVICES;
DEVELOPMENT METHODOLOGY;
HELICOPTER VIBRATION;
IDENTIFICATION MATRIX;
THEORETICAL CALCULATIONS;
VIBRATION REDUCTIONS;
ADVANCED VEHICLE CONTROL SYSTEMS;
HELICOPTERS;
FLIGHT CONTROL SYSTEMS;
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EID: 84883533669
PISSN: 15522938
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (6)
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References (0)
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