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    Helicopter Ground Resonance Phenomenon With Blade Stiffness Dissimilarities: Experimental and Theoretical Developments 

    Source: Journal of Vibration and Acoustics:;2013:;volume( 135 ):;issue: 005:;page 51028
    Author(s): Sanches, Leonardo; Michon, Guilhem; Berlioz, Alain; Alazard, Daniel
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recent works have studied ground resonance in helicopters under the aging or damage effects. Indeed, blade leadlag stiffness may vary randomly with time and differ from blade to blade. The influence of stiffness dissimilarities ...
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    Dynamic Modeling and Analysis of Spacecraft With Variable Tilt of Flexible Appendages 

    Source: Journal of Dynamic Systems, Measurement, and Control:;2014:;volume( 136 ):;issue: 002:;page 21020
    Author(s): Guy, Nicolas; Alazard, Daniel; Cumer, Christelle; Charbonnel, Catherine
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article describes a general framework to generate linearized models of satellites with large flexible appendages. The obtained model is parameterized according to the tilt of flexible appendages and can be used to ...
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    Flexible Multibody System Linear Modeling for Control Using Component Modes Synthesis and Double-Port Approach 

    Source: Journal of Dynamic Systems, Measurement, and Control:;2016:;volume( 138 ):;issue: 012:;page 121004
    Author(s): Perez, Jose Alvaro; Alazard, Daniel; Loquen, Thomas; Pittet, Christelle; Cumer, Christelle
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The main objective of this study is to propose a methodology for building a parametric linear model of flexible multibody systems (FMS) for control design. This new method uses a combined finite element (FE)–state-space ...
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    DSpace software copyright © 2002-2015  DuraSpace
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