Numerical simulation of a 3U-CubeSat orbit maintenance using electrothermal engine and magnetic attitude control system
- Authors: Roldugin D.S.1, Ivanov D.S.1, Tkachev S.S.1, Mashtakov Y.V.1, Khokhlov A.V.2, Starikov K.I.2,3
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Affiliations:
- Keldysh Institute of Applied Mathematics
- Geoscan Ltd.
- Saint-Petersburg State University
- Issue: Vol 63, No 2 (2025)
- Pages: 169-178
- Section: Articles
- URL: https://journal-vniispk.ru/0023-4206/article/view/294125
- DOI: https://doi.org/10.31857/S0023420625020043
- EDN: https://elibrary.ru/GOGXTV
- ID: 294125
Cite item
Abstract
The study focuses on performing orbit maintenance for a 3U-CubeSat using an electrothermal engine and a simple active magnetic attitude control system. The satellite is equipped with magnetorquers and a magnetometer. As such, it cannot maintain the engine axis attitude along the tangential direction for orbit maintenance. Instead, by realizing a constant dipole moment and damping, attitude along the geomagnetic induction vector is constructed. This attitude is close to tangential on a sun-synchronous orbit near the equator. Numerical simulation of the satellite motion is performed showing capability to provide simple and reliable orbit maintenance. Thrust parameters in uncontrolled motion are analyzed.
About the authors
D. S. Roldugin
Keldysh Institute of Applied Mathematics
Author for correspondence.
Email: rolduginds@gmail.com
Russian Federation, Moscow
D. S. Ivanov
Keldysh Institute of Applied Mathematics
Email: rolduginds@gmail.com
Russian Federation, Moscow
S. S. Tkachev
Keldysh Institute of Applied Mathematics
Email: rolduginds@gmail.com
Russian Federation, Moscow
Ya. V. Mashtakov
Keldysh Institute of Applied Mathematics
Email: rolduginds@gmail.com
Russian Federation, Moscow
A. V. Khokhlov
Geoscan Ltd.
Email: rolduginds@gmail.com
Russian Federation, Saint Petersburg
K. I. Starikov
Geoscan Ltd.; Saint-Petersburg State University
Email: rolduginds@gmail.com
Russian Federation, Saint Petersburg; Saint Petersburg
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