1. Identity statement | |
Reference Type | Journal Article |
Site | mtc-m21c.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 8JMKD3MGP3W34R/3RPN5K5 |
Repository | sid.inpe.br/mtc-m21c/2018/09.06.12.32 (restricted access) |
Last Update | 2020:09.16.20.06.13 (UTC) simone |
Metadata Repository | sid.inpe.br/mtc-m21c/2018/09.06.12.32.51 |
Metadata Last Update | 2021:02.11.18.10.44 (UTC) administrator |
ISSN | 0065-3438. |
Citation Key | SilvaGarcKugaZana:2018:SpAtEs |
Title | Spacecraft attitude estimation using unscented kalman filters, regularized particle filter and extended H filter |
Year | 2018 |
Access Date | 2024, Apr. 26 |
Type of Work | conference paper |
Secondary Type | PRE PI |
Number of Files | 1 |
Size | 1520 KiB |
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2. Context | |
Author | 1 Silva, William Reis 2 Garcia, Roberta V. 3 Kuga, Hélio Koiti 4 Zanardi, Maria Cecilia |
Resume Identifier | 1 2 3 8JMKD3MGP5W/3C9JHC9 |
Group | 1 2 3 DIDMC-CGETE-INPE-MCTIC-GOV-BR |
Affiliation | 1 Instituto Tecnologico de Aeronáutica (ITA) 2 Universidade de São Paulo (USP) 3 Instituto Nacional de Pesquisas Espaciais (INPE) 4 Universidade Federal do ABC (UFABC) |
Author e-Mail Address | 1 reis.william@gmail.com 2 robertagarcia@usp.br 3 helio.kuga@inpe.br 4 mceciliazanardi@gmail.com |
Journal | Advances in the Astronautical Sciences |
Volume | 162 |
Pages | 1195-1214 |
History (UTC) | 2018-09-06 12:33:22 :: simone -> administrator :: 2018 2019-02-22 20:42:09 :: administrator -> simone :: 2018 2020-09-16 20:06:13 :: simone -> administrator :: 2018 2021-02-11 18:10:44 :: administrator -> simone :: 2018 |
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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 |
Version Type | publisher |
Abstract | In this work, the attitude determination and the gyros drift estimation will be described for nonlinear systems using the Extended Kalman Filter (EKF), Extended H Filter (EHF), Second-Order Extended H Filter (SOEHF), Unscented Kalman Filter (UKF) and Regularized Particle Filter (RPF). An analysis of these estimation methods will be done, verifying which of them present better precision in such study. The attitude model is described by quaternions and the attitude sensors available are two DSS (Digital Sun Sensors), two IRES (Infrared Earth Sensor), and one triad of mechanical gyros. The application uses the simulated measurement data for orbit and attitude of the CBERS-2 (China Brazil Earth Resources Satellite) which has polar sun-synchronous orbit with an altitude of 778km, making about 14 revolutions per day. In this orbit, the satellite crosses the equator line always at the same local time, around 10:30 am. This dynamics allows the same conditions of solar illumination to be obtained during the acquisition of images. The simulated measurements of the CBERS-2 were provided by the inhouse package PROPAT, a Satellite Attitude and Orbit Toolbox for Matlab. The results in this work show that one can reach accuracies in attitude determination within the prescribed requirements, besides providing estimates of the gyro drifts which can be further used to enhance the gyro error model. |
Area | ETES |
Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Spacecraft attitude estimation... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | |
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4. Conditions of access and use | |
Language | en |
Target File | silva_artigo.pdf |
User Group | simone |
Reader Group | administrator simone |
Visibility | shown |
Read Permission | deny from all and allow from 150.163 |
Update Permission | not transferred |
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5. Allied materials | |
Next Higher Units | 8JMKD3MGPCW/446AF4B |
Citing Item List | sid.inpe.br/bibdigital/2021/02.11.18.06 4 sid.inpe.br/mtc-m21/2012/07.13.14.49.46 2 |
Dissemination | WEBSCI; PORTALCAPES; MGA; COMPENDEX. |
Host Collection | urlib.net/www/2017/11.22.19.04 |
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6. Notes | |
Empty Fields | alternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel doi e-mailaddress format isbn keywords label lineage mark mirrorrepository month nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url |
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7. Description control | |
e-Mail (login) | simone |
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