1. Identity statement | |
Reference Type | Conference Paper (Conference Proceedings) |
Site | mtc-m21d.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 8JMKD3MGP3W34T/4878APL |
Repository | sid.inpe.br/mtc-m21d/2022/12.13.17.09 |
Metadata Repository | sid.inpe.br/mtc-m21d/2022/12.13.17.09.34 |
Metadata Last Update | 2023:01.03.16.46.27 (UTC) administrator |
Secondary Key | INPE--PRE/ |
Citation Key | MurciaPiñerosVilhPrad:2022:InPeAe |
Title | Influence of periodic aerodynamic forces on the orbital elements of cubic satellites |
Year | 2022 |
Access Date | 2024, May 13 |
Secondary Type | PRE CN |
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2. Context | |
Author | 1 Murcia Piñeros, Jhonathan O. 2 Vilherna, R. de Moraes 3 Prado, Antonio Fernando Bertachini de Almeida |
Resume Identifier | 1 2 3 8JMKD3MGP5W/3C9JGJA |
Group | 1 2 3 DIMEC-CGCE-INPE-MCTI-GOV-BR |
Affiliation | 1 Universidade Federal de São Paulo (UNIFESP) 2 Universidade Federal de São Paulo (UNIFESP) 3 Instituto Nacional de Pesquisas Espaciais (INPE) |
Author e-Mail Address | 1 jhonathan.pineros@unifesp.br 2 3 antonio.prado@inpe.br |
Conference Name | Colóquio Brasileiro de Dinâmica Orbital, 221 |
Conference Location | 12-16 dez. 2022 |
Date | São José dos Campos, SP |
History (UTC) | 2022-12-13 17:09:34 :: simone -> administrator :: 2023-01-03 16:46:27 :: administrator -> simone :: 2022 |
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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 | Satellites in Low Earth Orbits are highly perturbed by the interaction with the atmosphere, which is the main non-gravitational perturbation (Miyata et al, 2014; Murcia et al, 2021). The two components of the aerodynamic force are the lift and drag, which initially are a function of the satellite geometry, materials, atmospheric and flow conditions. Due to the uncertainly in these values, traditional model search to fix the coefficients along the orbit lifetime (also known as canon ball model), without considering the changes due the flow direction (Prieto et al, 2014), product of the satellite attitude and rotational dynamics. The purpose of the present study is to analyze the influence of periodic variations of lift and drag on the orbital elements of a cubic satellite in Low Earth Orbit (LEO). For a practical approach, it is assumed the satellites in rotation at constant angular velocity. Three parallelepiped solids were selected to model the satellite geometry, which are similar in volume to the CubeSat standard The CubeSat population in LEO is increasing (Anz-Meador, 2015), and one advantage of those nanosats is that the uncertainty due to mass and dimensions are small. The aerodynamic coefficients are modeled using the panel method in free molecular flow, as a function of the angle of attack and the roll angle. For each solid, were selected two configurations in attitude at eight angular velocities. The effects of periodic variations in drag results in small secular perturbations in the orbital semi-major axis and eccentricity, with large differences at the lowest angular velocity. In the case of lift, the inclination is perturbed, and, at lower angular velocities, the effect is increased, because it keeps the magnitude and direction of this perturbation for a long time, however do not present significant perturbation from the mean orbit. The novelty of the study is the detection and quantification of the effects of periodic lift and drag in parallelepiped small satellites at Low Earth Orbits. |
Area | ETES |
Arrangement | urlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > Influence of periodic... |
doc Directory Content | there are no files |
source Directory Content | there are no files |
agreement Directory Content | |
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4. Conditions of access and use | |
Language | pt |
User Group | simone |
Visibility | shown |
Update Permission | not transferred |
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5. Allied materials | |
Next Higher Units | 8JMKD3MGPCW/46KTFK8 |
Host Collection | urlib.net/www/2021/06.04.03.40 |
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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 keywords label lineage mark mirrorrepository nextedition notes numberoffiles numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup readpermission rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle size sponsor subject targetfile tertiarymark tertiarytype type url volume |
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7. Description control | |
e-Mail (login) | simone |
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