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Dynamics and sensitivity analysis of a class of high speed aircraft

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Academic year: 2021

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Figure

Figure 2.1: GHAME Vehicle
Table 2.1: Geometric Properties of the GHAME Vehicle
Figure 2.2: Reentry Trajectory
Figure 3.1 illustrates the accuracy of the full GMS solution when compared to a numerical solution obtained using a fourth order Runge-Kutta integration in the case of a second order differential equation.
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