Sensitivity-analysis method for inverse simulation application (original) (raw)

Lu, Linghai, Murray-Smith, David and Thomson, D. G. ORCID logoORCID: https://orcid.org/0000-0003-3588-5710(2007) Sensitivity-analysis method for inverse simulation application.Journal of Guidance, Control, and Dynamics, 30(1), pp. 114-121. (doi: 10.2514/1.20722)

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Publisher's URL: http://dx.doi.org/10.2514/1.20722

Abstract

An important criticism of traditional methods of inverse simulation that are based on the Newton–Raphson algorithm is that they suffer from numerical problems. In this paper these problems are discussed and a new method based on sensitivity-analysis theory is developed and evaluated. The Jacobian matrix may be calculated by solving a sensitivity equation and this has advantages over the approximation methods that are usually applied when the derivatives of output variables with respect to inputs cannot be found analytically. The methodology also overcomes problems of input-output redundancy that arise in the traditional approaches to inverse simulation. The sensitivity- analysis approach makes full use of information within the time interval over which key quantities are compared, such as the difference between calculated values and the given ideal maneuver after each integration step. Applications to nonlinear HS125 aircraft and Lynx helicopter models show that, for this sensitivity-analysis method, more stable and accurate results are obtained than from use of the traditional Newton–Raphson approach.

Item Type: Articles
Status: Published
Refereed: Yes
Glasgow Author(s) Enlighten ID: Murray-Smith, Professor David and Thomson, Dr Douglas and Lu, Mr Linghai
Authors: Lu, L., Murray-Smith, D., and Thomson, D. G.
College/School: College of Science and Engineering > School of Engineering > Autonomous Systems and ConnectivityCollege of Science and Engineering > School of Engineering > Electronics and Nanoscale Engineering
Journal Name: Journal of Guidance, Control, and Dynamics
Publisher: American Institute of Aeronautics and Astronautics
ISSN: 0731-5090
ISSN (Online): 1533-3884
Copyright Holders: Copyright © 2006 American Institute of Aeronautics and Astronautics, Inc.
First Published: First published in Journal of Guidance, Control and Dynamics 30(1):114-121
Publisher Policy: Reproduced in accordance with the copyright policy of the publisher

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Funder and Project Information

1

Improved inverse simulation using nonlinear predictive methods

Douglas Thomson

GR/S91024/01

Aerospace Sciences

Deposit and Record Details

ID Code: 14622
Depositing User: Mr Adam Field
Datestamp: 19 Dec 2009 15:48
Last Modified: 01 May 2025 13:42
Date of first online publication: 1 January 2007
Date Deposited: 14 December 2015