The proposed effort is highly relevant to on-going and future NASA fixed wing projects, which involve innovative design concepts such as the Truss-Braced Wing, Blended Wing Body, and Supersonic Business Jet. The proposed work will offer a computational tool to the NASA designers for early exploration of design concepts that exploit the trade-off between the passive and active approaches for mitigating the potential aeroelastic problems associated with those configurations.
The proposed discrete time state-space plant model generation can be applied to various flight vehicles including blended wing-bodies, joined wings, sub/supersonic transports, morphing aircraft, and similar revolutionary concepts being pursued. The proposed research will be needed for designing the next generation of civil and military aircraft to meet the stringent future performance goals.
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