Developement of framework for structured uncertainty analysis for an aircraft

A. Iqbal; A. I. Bhatti

doi:10.1109/INMIC.2006.358208

Developement of framework for structured uncertainty analysis for an aircraft

A. Iqbal^*
, A. I. Bhatti

^*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

This paper provides a utility to find out the LTI model of an aircraft at any given operating point. The previous work provids only the spot linear models. The linear models obtained thorugh the numerical approach does not provide real dynamics of this sort of nonlinear models. The core of this paper is about analytical approach based on perturbation theory for linear model. The validity of the model is realized by the linear viz non-linear behavior about the operating point over which the perturbations were applied. The spot model verification strengthens the validity of the linearization framework which can be further used for determining the structure of the paramertic uncertainty for an aircraft model.

Original language	English
Title of host publication	10th IEEE International Multitopic Conference 2006, INMIC
Pages	444-450
Number of pages	7
DOIs	https://doi.org/10.1109/INMIC.2006.358208
State	Published - 2006
Externally published	Yes

Publication series

Name	10th IEEE International Multitopic Conference 2006, INMIC

ASJC Scopus subject areas

General Computer Science
Control and Systems Engineering

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10.1109/INMIC.2006.358208

Cite this

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title = "Developement of framework for structured uncertainty analysis for an aircraft",

abstract = "This paper provides a utility to find out the LTI model of an aircraft at any given operating point. The previous work provids only the spot linear models. The linear models obtained thorugh the numerical approach does not provide real dynamics of this sort of nonlinear models. The core of this paper is about analytical approach based on perturbation theory for linear model. The validity of the model is realized by the linear viz non-linear behavior about the operating point over which the perturbations were applied. The spot model verification strengthens the validity of the linearization framework which can be further used for determining the structure of the paramertic uncertainty for an aircraft model.",

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AB - This paper provides a utility to find out the LTI model of an aircraft at any given operating point. The previous work provids only the spot linear models. The linear models obtained thorugh the numerical approach does not provide real dynamics of this sort of nonlinear models. The core of this paper is about analytical approach based on perturbation theory for linear model. The validity of the model is realized by the linear viz non-linear behavior about the operating point over which the perturbations were applied. The spot model verification strengthens the validity of the linearization framework which can be further used for determining the structure of the paramertic uncertainty for an aircraft model.

UR - https://www.scopus.com/pages/publications/46449108021

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DO - 10.1109/INMIC.2006.358208

M3 - Conference contribution

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BT - 10th IEEE International Multitopic Conference 2006, INMIC

ER -

Developement of framework for structured uncertainty analysis for an aircraft

Abstract

Publication series

ASJC Scopus subject areas

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