https://murray.cds.caltech.edu/index.php?action=history&feed=atom&title=Fast_Mode_Switching_for_a_Thrust_Vectored_Aircraft 2026-09-06T19:26:08Z Revision history for this page on the wiki MediaWiki 1.44.2 https://murray.cds.caltech.edu/index.php?title=Fast_Mode_Switching_for_a_Thrust_Vectored_Aircraft&diff=20024&oldid=prev 2016-05-15T06:20:16Z

<p>htdb2wiki: creating page for 1996i_nm96-cesa.html</p> <p><b>New page</b></p><div>{{HTDB paper<br /> | authors = Michiel J. van Nieuwstadt and Richard M. Murray<br /> | title = Fast Mode Switching for a Thrust Vectored Aircraft<br /> | source = 1996 Multiconference on Computational Engineering in Systems Applications<br /> | year = 1996<br /> | type = Conference paper<br /> | funding = NSF/career, AFOSR/vehicles<br /> | url = http://www.cds.caltech.edu/~murray/preprints/nm96-cesa.pdf<br /> | abstract = <br /> Aircraft operate in different modes during flight, corresponding to different flight conditions and<br /> control schemes. We use differential flatness of an approximate model of the pitch dynamics of a<br /> thrust vectored aircraft to achieve fast switching between those modes. We investigate some<br /> methods to compensate for the perturbations to flatness. Simulations and experimental data are<br /> provided to validate the approach. <br /> <br /> | flags = NoRequest<br /> | tag = nm96-cesa<br /> | id = 1996i<br /> }}</div>

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