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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 This property is a special property in this wiki.
|
15 May 2016 06:20:16 + |
| URL This property is a special property in this wiki.
|
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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