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Faculté des Sciences appliquées
Faculté des Sciences appliquées
MASTER THESIS
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Master thesis and internship[BR]- Master's Thesis : Station-Keeping Attitude Control of an Under-Actuated CubeSat in orbit around Collinear Libation Points[BR]- Internship (linked to master's thesis)

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Macchiaiolo, Luca ULiège
Promotor(s) : Collette, Christophe ULiège
Date of defense : 7-Sep-2020/9-Sep-2020 • Permalink : http://hdl.handle.net/2268.2/10389
Details
Title : Master thesis and internship[BR]- Master's Thesis : Station-Keeping Attitude Control of an Under-Actuated CubeSat in orbit around Collinear Libation Points[BR]- Internship (linked to master's thesis)
Author : Macchiaiolo, Luca ULiège
Date of defense  : 7-Sep-2020/9-Sep-2020
Advisor(s) : Collette, Christophe ULiège
Committee's member(s) : Bruls, Olivier ULiège
Kerschen, Gaëtan ULiège
Language : English
Keywords : [fr] Station-Keeping
[fr] Attitude Control
[fr] CubeSat
[fr] Control Allocation
[fr] Libration point Orbits
[fr] Under-Actuated Spacecraft
Discipline(s) : Engineering, computing & technology > Aerospace & aeronautics engineering
Target public : Researchers
Professionals of domain
Student
Institution(s) : Université de Liège, Liège, Belgique
Politecnico di Milano, Milano, Italia
Degree: Master en ingénieur civil en aérospatiale, à finalité spécialisée en "aerospace engineering"
Faculty: Master thesis of the Faculté des Sciences appliquées

Abstract

[fr] The rising of the CubeSat concept is re-defning the canonical approach to
space mission design. The exponential interest in the use of CubeSats for deep
space missions opens up a wide range of new possibilities along with new technological
challenges. The reduced spacecraft available space combined with
stringent mission requirements drives the search for innovative solutions for
the optimization of the resources on board. On the other hand, new horizons
are opening up for CubeSat applications; Libration point missions for
scienti c or support purposes seem to be the next step in the development
and re nement of nano-satellite technologies. This work proposes an innovative
solution where the stand-alone CubeSat main propulsion system and the
ADCS actuators merge together in a 4-thruster assembly able to provide both
Station-Keeping and Attitude Control for Libration Point missions.


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Author

  • Macchiaiolo, Luca ULiège Université de Liège > Master ingé. civ. aérospat., à fin.

Promotor(s)

Committee's member(s)

  • Bruls, Olivier ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Laboratoire des Systèmes Multicorps et Mécatroniques
    ORBi View his publications on ORBi
  • Kerschen, Gaëtan ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux
    ORBi View his publications on ORBi
  • Total number of views 23
  • Total number of downloads 107










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