1. Identity statement | |
Reference Type | Conference Paper (Conference Proceedings) |
Site | mtc-m21b.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 8JMKD3MGP3W34P/3JL52BB |
Repository | sid.inpe.br/mtc-m21b/2015/06.09.15.24 |
Last Update | 2015:06.09.15.25.20 (UTC) administrator |
Metadata Repository | sid.inpe.br/mtc-m21b/2015/06.09.15.24.51 |
Metadata Last Update | 2018:06.04.02.55.27 (UTC) administrator |
Secondary Key | INPE--PRE/ |
Citation Key | SumidaCamLuzCruGoé:2015:FlDyPa |
Title | Flight dynamics parameter estimation of a rotary wing aircraft using theoutput error minimization with natural and meta heuristic methods |
Year | 2015 |
Access Date | 2024, May 17 |
Secondary Type | PRE CI |
Number of Files | 1 |
Size | 1026 KiB |
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2. Context | |
Author | 1 Sumida, Ivana Yoshie 2 Campos Velho, Haroldo Fraga de 3 Luz, Eduardo F. P. 4 Cruz, Ronaldo V. 5 Goés, Luiz Carlos S. |
Resume Identifier | 1 2 8JMKD3MGP5W/3C9JHC3 |
Group | 1 CAP-COMP-SPG-INPE-MCTI-GOV-BR 2 LAC-CTE-INPE-MCTI-GOV-BR |
Affiliation | 1 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 Address | 1 ivanayoshie@yahoo.com.br 2 haroldo@lac.inpe.br 3 4 5 goes@ita.br |
Conference Name | Pan-American Congress on Computational Mechanics, 1 (PANACM) |
Conference Location | Buenos Aires, Argentina |
Date | 29-29 Apr. |
History (UTC) | 2015-06-09 15:24:51 :: simone -> administrator :: 2018-06-04 02:55:27 :: administrator -> simone :: 2015 |
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3. Content and structure | |
Is the master or a copy? | is the master |
Content Stage | completed |
Transferable | 1 |
Content Type | External Contribution |
Keywords | Flight Simulation Parameter Identification Multiple Particle Collision Algorithm (MPCA) |
Abstract | Flight 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. |
Area | COMP |
Arrangement 1 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > Flight dynamics parameter... |
Arrangement 2 | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CAP > Flight dynamics parameter... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | |
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4. Conditions of access and use | |
data URL | http://mtc-m21b.sid.inpe.br/ibi/8JMKD3MGP3W34P/3JL52BB |
zipped data URL | http://mtc-m21b.sid.inpe.br/zip/8JMKD3MGP3W34P/3JL52BB |
Language | en |
User Group | simone |
Reader Group | administrator simone |
Visibility | shown |
Read Permission | allow from all |
Update Permission | not transferred |
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5. Allied materials | |
Mirror Repository | urlib.net/www/2011/03.29.20.55 |
Next Higher Units | 8JMKD3MGPCW/3ESGTTP 8JMKD3MGPCW/3F2PHGS |
Citing Item List | sid.inpe.br/bibdigital/2013/10.12.22.16 4 sid.inpe.br/mtc-m21/2012/07.13.14.49.40 3 |
Host Collection | sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 |
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6. Notes | |
Empty Fields | archivingpolicy 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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7. Description control | |
e-Mail (login) | simone |
update | |
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