Browse wiki

From MurrayWiki
Jump to: navigation, search
Stabilization of a Pitch Axis Flight Control Experiment with Input Rate Saturation
Abstract Motivated by problems in flight control, w …
Motivated by problems in flight control, we present a technique for stabilizing a chain of integrators in the presence of rate limitations on the input. Our technique improves on several existing techniques in the literature and has a number of interesting features. The controller is evaluated experimentally on a pitch axis flight control experiment at Caltech. The experimental results show that even in the presence of rate limits that cause a linear controller to go unstable, the time-varying controller stabilizes the system with minimal loss in performance.
e system with minimal loss in performance.  +
Authors Trygve Lauvdal and Richard M. Murray  +
ID 1997f  +
Source <i>Modeling, Identification and Control</i>, 20(4):225-240  +
Tag lm97-gnc  +
Title Stabilization of a Pitch Axis Flight Control Experiment with Input Rate Saturation +
Type Conference paper  +
Categories Papers
Modification date
This property is a special property in this wiki.
15 May 2016 06:19:59  +
URL
This property is a special property in this wiki.
http://www.cds.caltech.edu/~murray/preprints/lm97-gnc.pdf  +
hide properties that link here 
Stabilization of a Pitch Axis Flight Control Experiment with Input Rate Saturation + Title
 

 

Enter the name of the page to start browsing from.