| 1. Identity statement | |
| Reference Type | Book Section |
| Site | mtc-m16.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Repository | sid.inpe.br/marciana/2004/09.14.09.40 |
| Last Update | 2004:09.16.03.00.00 (UTC) administrator |
| Metadata Repository | sid.inpe.br/marciana/2004/09.14.09.40.45 |
| Metadata Last Update | 2021:02.11.18.09.27 (UTC) administrator |
| Secondary Key | INPE-11293-PRE/6730 |
| ISBN/ISSN | 85-17-00012-9 |
| Citation Key | RodriguesZana:2004:SpAtPr |
| Title | Spacecraft attitude propagation with different representations.  |
| Year | 2004 |
| Access Date | 2024, Dec. 27 |
| Secondary Type | PRE LI |
| Number of Files | 1 |
| Size | 389 KiB |
| 2. Context | |
| Author | 1 Rodrigues, Domingos Sávio dos Santos 2 Zanardi, Maria Cecília |
| Group | 1 DMC-INPE-MCT-BR |
| Affiliation | 1 Universidade Estadual Paulista, Departamento de Matemática, Grupo de Dinâmica Orbital e Planetologia (UNESP) 2 UNESP, Department of Mathematics, Group of Orbital Dynamics and Planetology |
| Editor | Kuga, Hélio Koiti |
| e-Mail Address | cecilia@feg.unesp.br |
| Book Title | Advances in space dynamics 4: celestial mechanics and astronautics |
| Publisher | INPE |
| City | São José dos Campos |
| Pages | 143-150 |
| History (UTC) | 2005-07-25 18:00:55 :: jefferson -> administrator :: 2021-02-11 18:09:27 :: administrator -> marciana :: 2004 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Keywords | SPACE MECHANICS AND CONTROL Spacecrafts Artificial satellites MECÂNICA ESPACIAL E CONTROLE Naves espaciais Satélites artificiais |
| Abstract | The objective of this paper is to analyze the dynamic equations of the rotational motion of an artificial satellite in terms of different representations (Euler angles, Andoyer variables and quaternion). The external torques are not included in this study. Analytical solutions are presented for symmetrical satellites when the equation of motion are described in terms of the Andoyer variable or Euler angles and angular velocity. A semi-analytical solution is proposed for symmetrical satellite when the equations are described by quaternion. When compared, numerical and semi-analytical solutions have a good agreement during the time range considered. A numerical solution is presented for no symmetrical satellites when the motion equation are described by angular velocity and quaternion. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Spacecraft attitude propagation... |
| doc Directory Content | access |
| source Directory Content | there are no files |
| agreement Directory Content | there are no files |
| 4. Conditions of access and use | |
| data URL | http://urlib.net/ibi/sid.inpe.br/marciana/2004/09.14.09.40 |
| zipped data URL | http://urlib.net/zip/sid.inpe.br/marciana/2004/09.14.09.40 |
| Language | en |
| Target File | Spacecraft attitude.pdf |
| User Group | administrator jefferson |
| Visibility | shown |
| Copy Holder | SID/SCD |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Citing Item List | sid.inpe.br/bibdigital/2021/02.11.18.06 16 |
| Dissemination | NTRSNASA, BNDEPOSITOLEGAL. |
| Host Collection | sid.inpe.br/banon/2003/08.15.17.40 |
| 6. Notes | |
| Empty Fields | archivingpolicy archivist callnumber contenttype copyright creatorhistory descriptionlevel documentstage doi edition electronicmailaddress format identifier isbn issn label lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup readpermission resumeid rightsholder schedulinginformation secondarydate secondarymark serieseditor seriestitle session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |