2008
DOI: 10.2514/1.32799
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Structure Computation of Quiet Spike Flight-Test Data During Envelope Expansion

Abstract: System identification or mathematical modeling is used in the aerospace community for development of simulation models for robust control law design. These models are often described as linear time-invariant processes. Nevertheless, it is well known that the underlying process is often nonlinear. The reason for using a linear approach has been due to the lack of a proper set of tools for the identification of nonlinear systems. Over the past several decades, the controls and biomedical communities have made gr… Show more

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