Nonlinear Dynamic Inversion Based Anti-windup: An Aerospace Application

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

doi:10.3182/20080706-5-KR-1001.02400

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 proceeding › Conference contribution › peer-review

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.

Original language	English
Title of host publication	IFAC Proceedings Volumes Issue 2, 2008
Pages	14156-14161
Number of pages	6
Volume	41
DOIs	https://doi.org/10.3182/20080706-5-KR-1001.02400
Publication status	Published - 2008

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title = "Nonlinear Dynamic Inversion Based Anti-windup: An Aerospace Application",

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.",

author = "PP Menon and G Herrmann and MC Turner and MH Lowenberg and DC Bates and I Postlethwaite",

note = "Conference Organiser: IFAC",

year = "2008",

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AU - Menon, PP

AU - Herrmann, G

AU - Turner, MC

AU - Lowenberg, MH

AU - Bates, DC

AU - Postlethwaite, I

N1 - Conference Organiser: IFAC

PY - 2008

Y1 - 2008

N2 - 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.

AB - 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.

U2 - 10.3182/20080706-5-KR-1001.02400

DO - 10.3182/20080706-5-KR-1001.02400

M3 - Conference contribution

VL - 41

SP - 14156

EP - 14161

BT - IFAC Proceedings Volumes Issue 2, 2008

ER -

Nonlinear Dynamic Inversion Based Anti-windup: An Aerospace Application

Abstract

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