Nonlinear Dynamic Inversion Based Anti-windup - An Aerospace Application

PP Menon, G Herrmann, MC Turner, MH Lowenberg, DC Bates, I Postlethwaite

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

1 Citation (Scopus)

Abstract

A recently suggested general anti-windup (AW) compensation scheme is applied to the nonlinear simulation model of the 1/16 scaled BAe Hawk aircraft model used for wind tunnel experiments. The Hawk is modelled as a nonlinear affine system subject to input constraints and has a primary control system consisting of an inner-loop nonlinear dynamic inversion controller and an outer-loop linear PID controller. To address the input constraints a recently introduced nonlinear L2 sub-optimal AW compensation method is applied and compared with a nonlinear version of the internal model control AW scheme. Nonlinear simulation results demonstrate the promise of the approach and indicate the superiority of the optimal AW scheme.
Translated title of the contributionNonlinear Dynamic Inversion Based Anti-windup - An Aerospace Application
Original languageEnglish
Title of host publication17th IFAC World Congress, Seoul, Korea
Pages14156 - 14161
DOIs
Publication statusPublished - 2008

Bibliographical note

Conference Organiser: IFAC

Fingerprint Dive into the research topics of 'Nonlinear Dynamic Inversion Based Anti-windup - An Aerospace Application'. Together they form a unique fingerprint.

Cite this