Development of Adaptive Seat Mounts for Helicopter Aircrew Body Vibration Reduction
Author:
Affiliation:
1. Institute for Aerospace Research, National Research Council, Ottawa, Canada, K1A0R6,
2. Institute for Aerospace Research, National Research Council, Ottawa, Canada, K1A0R6
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Mechanics of Materials,Aerospace Engineering,Automotive Engineering,General Materials Science
Link
http://journals.sagepub.com/doi/pdf/10.1177/1077546309103275
Reference14 articles.
1. A Two-Stage Vibration Isolation System Featuring an Electrorheological Damper via the Semi-Active Static Output Feedback Variable Structure Control Method
2. Wind Tunnel Test of a Smart Rotor Model with Individual Blade Twist Control
3. Smart Spring Impedance Control Algorithm for Helicopter Blade Harmonic Vibration Suppression
4. Use of random noise for on‐line transducer modeling in an adaptive active attenuation system
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