Lyapunov-Based Control via Atmospheric Drag for Tetrahedral Satellite Formation

The problem of small tetrahedral satellite formation maintenance in a Low Earth Orbit is being considered. The main purpose is to develop a simple algorithm for tetrahedron control via atmospheric drag. To design a controller, the direct Lyapunov method is used. The control obtained is suitable for...

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Main Authors: Mikhail Ovchinnikov, Yaroslav Mashtakov, Sergey Shestakov
Format: Article
Language:English
Published: MDPI AG 2024-01-01
Series:Mathematics
Subjects:
Online Access:https://www.mdpi.com/2227-7390/12/2/189
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author Mikhail Ovchinnikov
Yaroslav Mashtakov
Sergey Shestakov
author_facet Mikhail Ovchinnikov
Yaroslav Mashtakov
Sergey Shestakov
author_sort Mikhail Ovchinnikov
collection DOAJ
description The problem of small tetrahedral satellite formation maintenance in a Low Earth Orbit is being considered. The main purpose is to develop a simple algorithm for tetrahedron control via atmospheric drag. To design a controller, the direct Lyapunov method is used. The control obtained is suitable for tetrahedral formation maintenance, with an average distance of about 1 km. During the controlled motion, the geometric characteristics of the tetrahedron are preserved.
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spelling doaj.art-5fcf6d2908384fdb822fea5d76dc78152024-01-26T17:31:01ZengMDPI AGMathematics2227-73902024-01-0112218910.3390/math12020189Lyapunov-Based Control via Atmospheric Drag for Tetrahedral Satellite FormationMikhail Ovchinnikov0Yaroslav Mashtakov1Sergey Shestakov2Keldysh Institute of Applied Mathematics of RAS, Miusskaya Sq. 4, 125047 Moscow, RussiaKeldysh Institute of Applied Mathematics of RAS, Miusskaya Sq. 4, 125047 Moscow, RussiaKeldysh Institute of Applied Mathematics of RAS, Miusskaya Sq. 4, 125047 Moscow, RussiaThe problem of small tetrahedral satellite formation maintenance in a Low Earth Orbit is being considered. The main purpose is to develop a simple algorithm for tetrahedron control via atmospheric drag. To design a controller, the direct Lyapunov method is used. The control obtained is suitable for tetrahedral formation maintenance, with an average distance of about 1 km. During the controlled motion, the geometric characteristics of the tetrahedron are preserved.https://www.mdpi.com/2227-7390/12/2/189tetrahedral formationLyapunov controlatmospheric drag
spellingShingle Mikhail Ovchinnikov
Yaroslav Mashtakov
Sergey Shestakov
Lyapunov-Based Control via Atmospheric Drag for Tetrahedral Satellite Formation
Mathematics
tetrahedral formation
Lyapunov control
atmospheric drag
title Lyapunov-Based Control via Atmospheric Drag for Tetrahedral Satellite Formation
title_full Lyapunov-Based Control via Atmospheric Drag for Tetrahedral Satellite Formation
title_fullStr Lyapunov-Based Control via Atmospheric Drag for Tetrahedral Satellite Formation
title_full_unstemmed Lyapunov-Based Control via Atmospheric Drag for Tetrahedral Satellite Formation
title_short Lyapunov-Based Control via Atmospheric Drag for Tetrahedral Satellite Formation
title_sort lyapunov based control via atmospheric drag for tetrahedral satellite formation
topic tetrahedral formation
Lyapunov control
atmospheric drag
url https://www.mdpi.com/2227-7390/12/2/189
work_keys_str_mv AT mikhailovchinnikov lyapunovbasedcontrolviaatmosphericdragfortetrahedralsatelliteformation
AT yaroslavmashtakov lyapunovbasedcontrolviaatmosphericdragfortetrahedralsatelliteformation
AT sergeyshestakov lyapunovbasedcontrolviaatmosphericdragfortetrahedralsatelliteformation