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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3JL52BB
Repositorysid.inpe.br/mtc-m21b/2015/06.09.15.24
Last Update2015:06.09.15.25.20 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2015/06.09.15.24.51
Metadata Last Update2018:06.04.02.55.27 (UTC) administrator
Secondary KeyINPE--PRE/
Citation KeySumidaCamLuzCruGoé:2015:FlDyPa
TitleFlight dynamics parameter estimation of a rotary wing aircraft using theoutput error minimization with natural and meta heuristic methods
Year2015
Access Date2024, May 17
Secondary TypePRE CI
Number of Files1
Size1026 KiB
2. Context
Author1 Sumida, Ivana Yoshie
2 Campos Velho, Haroldo Fraga de
3 Luz, Eduardo F. P.
4 Cruz, Ronaldo V.
5 Goés, Luiz Carlos S.
Resume Identifier1
2 8JMKD3MGP5W/3C9JHC3
Group1 CAP-COMP-SPG-INPE-MCTI-GOV-BR
2 LAC-CTE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3
4 Instituto Tecnológico de Aeronáutica (ITA)
5 Instituto Tecnológico de Aeronáutica (ITA)
Author e-Mail Address1 ivanayoshie@yahoo.com.br
2 haroldo@lac.inpe.br
3
4
5 goes@ita.br
Conference NamePan-American Congress on Computational Mechanics, 1 (PANACM)
Conference LocationBuenos Aires, Argentina
Date29-29 Apr.
History (UTC)2015-06-09 15:24:51 :: simone -> administrator ::
2018-06-04 02:55:27 :: administrator -> simone :: 2015
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsFlight Simulation
Parameter Identification
Multiple Particle Collision Algorithm (MPCA)
AbstractFlight simulators are employed by civil and military pilots, as well by engineers, in order to increase the security in training of crew, and to find out the behavior of the aircraft under different operational conditions. However, it is necessary to calibrate the simulator software to have good adherence to real flight. In this process, parameters of the mathematical model of the flight simulation need to be identified, such that the simulation is as close as possible to the real flight dynamic. With appropriated values of these parameters, the simulator will be ready for training or assessing the aircraft dynamics. This can be described as an inverse problem or parameter identification, formulated as an optimization problem. The simulator is designed to represent the dynamics of the helicopter AS355-F2, for testing two types of maneuvers were employed: a sinusoidal input and 3-2-1-1 pulse input. The aerodynamics derivatives estimation methodology is also known as quad-M scheme, since it involves four different processes: Measurement, Maneuver, Model, and Methods of error minimization. The tested helicopter was equipped with the Aydin Vector Data Acquisition System (AVDAS) PCU-816-I, ATD-800 digital recorder The system measures a total of thirty-five different parameters. The calibration of a dynamic flight simulator is achieved by two meta-heuristics: a Genetic Algorithm and a new approach named Multiple Particle Collision Algorithm (MPCA). Preliminary results show a good performance of the employed optimization methods.
AreaCOMP
Arrangement 1urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > Flight dynamics parameter...
Arrangement 2urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CAP > Flight dynamics parameter...
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4. Conditions of access and use
data URLhttp://mtc-m21b.sid.inpe.br/ibi/8JMKD3MGP3W34P/3JL52BB
zipped data URLhttp://mtc-m21b.sid.inpe.br/zip/8JMKD3MGP3W34P/3JL52BB
Languageen
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/3ESGTTP
8JMKD3MGPCW/3F2PHGS
Citing Item Listsid.inpe.br/bibdigital/2013/10.12.22.16 4
sid.inpe.br/mtc-m21/2012/07.13.14.49.40 3
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsarchivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn label lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject targetfile tertiarymark tertiarytype type url versiontype volume
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