LMIs in Control/Applications/F16 Longitudinal Stabilitzation: Revision history

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20 November 2021

  • curprev 02:5102:51, 20 November 2021 imported>Jtstoffel 3,934 bytes +3,934 Created page with "<big><big>'''F-16 Longitudinal Stabilization using Hinf Output Feedback'''</big></big> The linearized longitudinal dynamics of the F-16 aircraft are considered in this example. The nonlinear 6DOF model is linearized using straight-and-level flight conditions of: <math> \begin{align} V = 502 ft/s \\ \bar{q} = 300psf \\ X_{cg} = 0.35\bar{c} \\ \delta_{trim} = -0.7588deg \end{align} </math> See chapter 3 of [] for further details. == '''The System''' == The state-spac..."
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