Browse wiki
From MurrayWiki
Rapid Hover to Forward Flight Transitions for a Thrust Vectored Aircraft |
Abstract |
This paper investigates the use of efficie … This paper investigates the use of efficient computational algorithms for the
computation of a nominal trajectory for fast transition between flight modes. We use
differential flatness of an approximate model of the longitudinal dynamics of a thrust
vectored aircraft to achieve fast switching between flight modes. We investigate some
methods to compensate for the discrepancy between the full aerodynamic model and the
approximate flat model, and analyze their performance. Simulations and experimental data
for a thrust vectored flight control experiment at Caltech are provided to validate the
approach. ech are provided to validate the
approach. +
|
---|---|
Authors | Michiel J. van Nieuwstadt and Richard M. Murray + |
ID | 1996o + |
Source | <i>J. Guidance, Control, and Dynamics</i>, 21(1):93-100, Jan-Feb 1998 + |
Tag | nm96-jgcd + |
Title | Rapid Hover to Forward Flight Transitions for a Thrust Vectored Aircraft + |
Type | Preprint + |
Categories | Papers |
Modification date This property is a special property in this wiki.
|
15 May 2016 06:20:11 + |
URL This property is a special property in this wiki.
|
http://www.cds.caltech.edu/~murray/preprints/nm96-jgcd.pdf + |
hide properties that link here |
Rapid Hover to Forward Flight Transitions for a Thrust Vectored Aircraft + | Title |
---|