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    A Hybrid Autonomous Control Approach 

    Source: Journal of Dynamic Systems, Measurement, and Control:;1995:;volume( 117 ):;issue: 002:;page 232
    Author(s): Robert L. Clark
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A hybrid autonomous control approach for active damping and control of a persistent disturbance is presented. Direct velocity feedback control is coupled with an adaptive feedforward controller ...
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    Active Control of Low Frequency Modes in an Aircraft Fuselage Using Spatially Weighted Arrays 

    Source: Journal of Vibration and Acoustics:;2000:;volume( 122 ):;issue: 003:;page 227
    Author(s): Steven A. Lane; Robert L. Clark; Steve C. Southward
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Acoustic enclosures such as aircraft cabins often display lightly damped modal behavior at low frequencies where passive treatments are impractical due to mass and volume constraints. This work ...
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    A Comprehensive Study of the RL Series Resonant Shunted Piezoelectric: A Feedback Controls Perspective 

    Source: Journal of Vibration and Acoustics:;2011:;volume( 133 ):;issue: 001:;page 11012
    Author(s): Matthew V. Kozlowski; Daniel G. Cole; Robert L. Clark
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The resonant shunted piezoelectric has been shown a viable solution for stable vibration control. Two main implementations of the single mode shunt circuit have been developed; the original with ...
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    Genetic Spatial Optimization of Active Elements on an Aeroelastic Delta Wing 

    Source: Journal of Vibration and Acoustics:;2001:;volume( 123 ):;issue: 004:;page 466
    Author(s): Robert E. Richard; Research Assistant; John A. Rule; Robert L. Clark
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This work outlines a cohesive approach for the design and implementation of a genetically optimized, active aeroelastic delta wing. Emphasis was placed on computational efficiency of model ...
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