TY - BOOK ID - 145171367 TI - Active vibration control for helicopter interior noise reduction using power minimization AU - Mendoza, J. AU - Langley Research Center AU - United States. PY - 2014 PB - Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, DB - UniCat KW - Noise reduction. KW - Rotary wing aircraft. KW - Aircraft compartments. KW - Optimal control. KW - Structural vibration. KW - Vibration damping. UR - https://www.unicat.be/uniCat?func=search&query=sysid:145171367 AB - ER -