]> 2026-07-06T20:52:18+00:00 Fast Mode Switching for a Thrust Vectored Aircraft 0 en Aircraft operate in different modes during flight, corresponding to different flight conditions and control schemes. We use differential flatness of an approximate model of the pitch dynamics of a thrust vectored aircraft to achieve fast switching between those modes. We investigate some methods to compensate for the perturbations to flatness. Simulations and experimental data are provided to validate the approach. Michiel J. van Nieuwstadt and Richard M. Murray NoRequest 1996i 1996 Multiconference on Computational Engineering in Systems Applications nm96-cesa Conference paper 2016-05-15T06:20:16Z 2457523.7640741 Fast Mode Switching for a Thrust Vectored Aircraft Title 102 en Title