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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m21d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34T/475T7G8
Repositorysid.inpe.br/mtc-m21d/2022/06.22.15.19
Metadata Repositorysid.inpe.br/mtc-m21d/2022/06.22.15.19.48
Metadata Last Update2023:01.03.16.46.08 (UTC) administrator
Secondary KeyINPE--PRE/
Citation KeyFagondeSantPrad:2022:AtCoSa
TitleAttitude-Based Control of Satellite Formations Using Aerodynamic Forces and Solar Radiation Pressure
Year2022
Access Date2024, May 14
Secondary TypePRE CI
2. Context
Author1 Fagonde, Caio
2 Santos, Willer
3 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JGJA
Group1
2
3 DIMEC-CGCE-INPE-MCTI-GOV-BR
Affiliation1 Universidade Federal do ABC (UFABC)
2 Instituto Tecnológico da Aeronáutica (ITA)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2
3 antonio.prado@inpe.br
Conference NameInternational Workshop on Satellite Constellations and Forming Flying (IWSCFF), 11
Conference LocationMilano, Italy
Date7-10 June 2022
History (UTC)2022-06-22 15:20:22 :: simone -> administrator :: 2022
2023-01-03 16:46:08 :: administrator -> simone :: 2022
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsFormation Flying missions
Constellation missions
Earth-bounded Missions
AbstractThe exploitation of natural environmental forces as an alternative means of satellite control is an enabling technology that increases the feasibility range of small satellite operations when the performance of continuous station-keeping or reconfiguration maneuvers is required. On a Low Earth Orbit, for instance, differential atmospheric drag accelerations that arise due to small differences in attitude, mass or exposed surface area between satellites in otherwise nearly identical trajectories can be used as a phasing mechanism [1] or for implementing rendezvous maneuvers in satellite formations [2]. On higher orbits, forces such as those created by solar radiation pressure can be used to generate differential accelerations between the members of a satellite formation [3]. This work aims to analyze the simultaneous use of aerodynamic forces, including both differential lift and differential drag, and solar radiation pressure as a means of satellite formation control, including full attitude dynamics and a Lyapunov-based control system for reference tracking. Historically, the idea of using differential aerodynamic forces in satellite formations can be traced back to the work of Carolina L. Leonard [4], who proposed the use of differential drag for satellite formation control, using the linearized relative motion model of the Hill-Clohessy-Wiltshire equations. In this case, the acting drag force was controlled by drag plates that could be rotated in order to adjust the magnitude of the acceleration. This idea would be further explored by various authors, such as Kumar and Ng [5], Bevilacqua and Romano [6], and Lambert et al. [7]. The use of differential lift, on the other hand, was often neglected due to the lift forces being orders of magnitude smaller than the atmospheric drag, in most circumstances. Horsley [8], however, proposed the use of lift in order to control the out-of-plane motion of each satellite, developing an algorithm for satellite rendezvous. Horsleys algorithm would be further improved by Shao et al. [9] and Smith et al. [10], removing certain collision risks present in the original algorithm. Other studies further contemplated the simultaneous use of differential lift and drag.
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User Groupsimone
Reader Groupadministrator
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Visibilityshown
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/46KTFK8
Host Collectionurlib.net/www/2021/06.04.03.40
6. Notes
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