Flight Path Reconstruction and Parameter Estimation Using Output-Error Method

This work describes the application of the output-error method using the Levenberg-Marquardt optimization algorithm to the Flight Path Reconstruction (FPR) problem, which constitutes an important preliminary step towards the aircraft parameter identification. This method is also applied to obtain th...

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Main Authors: Benedito Carlos de Oliveira Maciel, Luiz Carlos Sandoval Góes, Elder Moreira Hemerly, Nei Salis Brasil Neto
Format: Article
Language:English
Published: Wiley 2006-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.1155/2006/960391
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author Benedito Carlos de Oliveira Maciel
Luiz Carlos Sandoval Góes
Elder Moreira Hemerly
Nei Salis Brasil Neto
author_facet Benedito Carlos de Oliveira Maciel
Luiz Carlos Sandoval Góes
Elder Moreira Hemerly
Nei Salis Brasil Neto
author_sort Benedito Carlos de Oliveira Maciel
collection DOAJ
description This work describes the application of the output-error method using the Levenberg-Marquardt optimization algorithm to the Flight Path Reconstruction (FPR) problem, which constitutes an important preliminary step towards the aircraft parameter identification. This method is also applied to obtain the aerodynamic and control derivatives of a regional jet aircraft from flight test data with measurement noise and bias. Experimental results are reported, employing a real jet aircraft, with flight test data acquired by smart probes, inertial sensors (gyrometers and accelerometers) and Global Positioning Systems (GPS) receivers.
format Article
id doaj-art-b210b7a0dee04b938c7a9fae2f102da7
institution Kabale University
issn 1070-9622
1875-9203
language English
publishDate 2006-01-01
publisher Wiley
record_format Article
series Shock and Vibration
spelling doaj-art-b210b7a0dee04b938c7a9fae2f102da72025-02-03T06:11:40ZengWileyShock and Vibration1070-96221875-92032006-01-01134-537939210.1155/2006/960391Flight Path Reconstruction and Parameter Estimation Using Output-Error MethodBenedito Carlos de Oliveira Maciel0Luiz Carlos Sandoval Góes1Elder Moreira Hemerly2Nei Salis Brasil Neto3Department of Aeronautical-Mechanical Engineering, Technological Institute of Aeronautics, 12228-900, São José dos Campos, SP, BrazilDepartment of Aeronautical-Mechanical Engineering, Technological Institute of Aeronautics, 12228-900, São José dos Campos, SP, BrazilDivision of Electronic Engineering, Technological Institute of Aeronautics, 12228-900, São José dos Campos, SP, BrazilDepartment of Aeronautical-Mechanical Engineering, Technological Institute of Aeronautics, 12228-900, São José dos Campos, SP, BrazilThis work describes the application of the output-error method using the Levenberg-Marquardt optimization algorithm to the Flight Path Reconstruction (FPR) problem, which constitutes an important preliminary step towards the aircraft parameter identification. This method is also applied to obtain the aerodynamic and control derivatives of a regional jet aircraft from flight test data with measurement noise and bias. Experimental results are reported, employing a real jet aircraft, with flight test data acquired by smart probes, inertial sensors (gyrometers and accelerometers) and Global Positioning Systems (GPS) receivers.http://dx.doi.org/10.1155/2006/960391
spellingShingle Benedito Carlos de Oliveira Maciel
Luiz Carlos Sandoval Góes
Elder Moreira Hemerly
Nei Salis Brasil Neto
Flight Path Reconstruction and Parameter Estimation Using Output-Error Method
Shock and Vibration
title Flight Path Reconstruction and Parameter Estimation Using Output-Error Method
title_full Flight Path Reconstruction and Parameter Estimation Using Output-Error Method
title_fullStr Flight Path Reconstruction and Parameter Estimation Using Output-Error Method
title_full_unstemmed Flight Path Reconstruction and Parameter Estimation Using Output-Error Method
title_short Flight Path Reconstruction and Parameter Estimation Using Output-Error Method
title_sort flight path reconstruction and parameter estimation using output error method
url http://dx.doi.org/10.1155/2006/960391
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AT luizcarlossandovalgoes flightpathreconstructionandparameterestimationusingoutputerrormethod
AT eldermoreirahemerly flightpathreconstructionandparameterestimationusingoutputerrormethod
AT neisalisbrasilneto flightpathreconstructionandparameterestimationusingoutputerrormethod