Two-stage Active Disturbance Rejection Control in aerospace applications: The case of an orbit transfer for a point mass satellite

Technological advances have led to the development of smaller and more efficient satellites, which have gained popularity in various fields including education, research, and communications. However, disturbances such as gravitational forces, atmospheric drag, and space debris may affect their orbit...

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Bibliographic Details
Published in2023 20th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE) pp. 1 - 6
Main Authors Aguilar-Orduna, Mario Andres, Sira-Ramirez, Hebertt Jose, Gomez-Leon, Brian Camilo, Garrido-Moctezuma, Ruben Alejandro
Format Conference Proceeding
LanguageEnglish
Published IEEE 25.10.2023
Subjects
Active Disturbance Rejection Control
Aerodynamics
aerospace applications
Input variables
Orbits
Robust control
Small satellites
Space debris
Systems engineering and theory
underactuated systems
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Summary:Technological advances have led to the development of smaller and more efficient satellites, which have gained popularity in various fields including education, research, and communications. However, disturbances such as gravitational forces, atmospheric drag, and space debris may affect their orbits. This article proposes a two-stage Active Disturbance Rejection Control (ADRC) approach for the orbit transfer of small satellites. The paper presents the control design procedure and showcases numerical simulations, demonstrating the technique's effectiveness in the particular case of study.
ISSN:2642-3766
DOI:10.1109/CCE60043.2023.10332871