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Nonlinear model order reduction and control of very flexible aircraft

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Figure

Figure 1.1: NASA Helios unmanned aerial vehicle as in Ref. [1]
Figure 1.2: NASA Helios flight accident as in [1]
Figure 1.3: Computational cost with respect to the degrees–of–freedom to capture 1 s of anunsteady flight dynamic calculation with strip aerodynamics and CFD
Figure 1.5: Panelling scheme for the UVLM as in [51]
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