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Fast Mode Switching for a Thrust Vectored Aircraft
Abstract Aircraft operate in different modes during …
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.
ata are provided to validate the approach.  +
Authors Michiel J. van Nieuwstadt and Richard M. Murray  +
Flags NoRequest  +
ID 1996i  +
Source 1996 Multiconference on Computational Engineering in Systems Applications  +
Tag nm96-cesa  +
Title Fast Mode Switching for a Thrust Vectored Aircraft +
Type Conference paper  +
Categories Papers
Modification date
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15 May 2016 06:20:16  +
URL
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http://www.cds.caltech.edu/~murray/preprints/nm96-cesa.pdf  +
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Fast Mode Switching for a Thrust Vectored Aircraft + Title
 

 

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