Geometric Nonlinearities of Aircraft Systems

B. Krauskopf; P. Thota; M. Lowenberg

doi:10.1007/978-3-642-12110-4_23

Geometric Nonlinearities of Aircraft Systems

B. Krauskopf
, P. Thota
, M. Lowenberg

Cabot Institute for the Environment

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

Abstract

Nonlinearities due to geometric effects; in particular, via angular variables that are not small, are important for aircraft operation. Geometric nonlinearities have a strong effect on the dynamics of the aircraft system under consideration, and they are especially pronounced in aircraft ground operations. As a concrete example we consider here the effect of a non-zero rake angle on the dynamics of a nose landing gear. More specifically, we use tools from bifurcation theory to investigate the stability of the straight-rolling motion during a take-off run.

Original language	English
Title of host publication	PROGRESS IN INDUSTRIAL MATHEMATICS AT ECMI 2008
Editors	AD Fitt, J Norbury, H Ockendon, RE Wilson
Place of Publication	BERLIN
Publisher	Springer-Verlag Berlin
Pages	181-186
Number of pages	6
ISBN (Print)	978-3-642-12109-8
DOIs	https://doi.org/10.1007/978-3-642-12110-4_23
Publication status	Published - 2010
Event	15th European Conference on Mathematics for Industry - London, United Kingdom Duration: 30 Jun 2008 → 4 Jul 2008

Conference

Conference	15th European Conference on Mathematics for Industry
Country/Territory	United Kingdom
City	London
Period	30/06/08 → 4/07/08

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@inproceedings{ddf3fbfd8c434ba3bc0d57a72e5c8846,

title = "Geometric Nonlinearities of Aircraft Systems",

abstract = "Nonlinearities due to geometric effects; in particular, via angular variables that are not small, are important for aircraft operation. Geometric nonlinearities have a strong effect on the dynamics of the aircraft system under consideration, and they are especially pronounced in aircraft ground operations. As a concrete example we consider here the effect of a non-zero rake angle on the dynamics of a nose landing gear. More specifically, we use tools from bifurcation theory to investigate the stability of the straight-rolling motion during a take-off run.",

author = "B. Krauskopf and P. Thota and M. Lowenberg",

year = "2010",

doi = "10.1007/978-3-642-12110-4\_23",

language = "English",

isbn = "978-3-642-12109-8",

pages = "181--186",

editor = "AD Fitt and J Norbury and H Ockendon and RE Wilson",

booktitle = "PROGRESS IN INDUSTRIAL MATHEMATICS AT ECMI 2008",

publisher = "Springer-Verlag Berlin",

note = "15th European Conference on Mathematics for Industry ; Conference date: 30-06-2008 Through 04-07-2008",

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TY - GEN

T1 - Geometric Nonlinearities of Aircraft Systems

AU - Krauskopf, B.

AU - Thota, P.

AU - Lowenberg, M.

PY - 2010

Y1 - 2010

N2 - Nonlinearities due to geometric effects; in particular, via angular variables that are not small, are important for aircraft operation. Geometric nonlinearities have a strong effect on the dynamics of the aircraft system under consideration, and they are especially pronounced in aircraft ground operations. As a concrete example we consider here the effect of a non-zero rake angle on the dynamics of a nose landing gear. More specifically, we use tools from bifurcation theory to investigate the stability of the straight-rolling motion during a take-off run.

AB - Nonlinearities due to geometric effects; in particular, via angular variables that are not small, are important for aircraft operation. Geometric nonlinearities have a strong effect on the dynamics of the aircraft system under consideration, and they are especially pronounced in aircraft ground operations. As a concrete example we consider here the effect of a non-zero rake angle on the dynamics of a nose landing gear. More specifically, we use tools from bifurcation theory to investigate the stability of the straight-rolling motion during a take-off run.

U2 - 10.1007/978-3-642-12110-4_23

DO - 10.1007/978-3-642-12110-4_23

M3 - Conference Contribution (Conference Proceeding)

SN - 978-3-642-12109-8

SP - 181

EP - 186

BT - PROGRESS IN INDUSTRIAL MATHEMATICS AT ECMI 2008

A2 - Fitt, AD

A2 - Norbury, J

A2 - Ockendon, H

A2 - Wilson, RE

PB - Springer-Verlag Berlin

CY - BERLIN

T2 - 15th European Conference on Mathematics for Industry

Y2 - 30 June 2008 through 4 July 2008

ER -

Geometric Nonlinearities of Aircraft Systems

Abstract

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