Monoaxial Electrodynamic Stabilization of an Artificial Earth Satellite in the Orbital Coordinate System via Control With Distributed Delay

Monoaxial Electrodynamic Stabilization of an Artificial Earth Satellite in the Orbital Coordinate System via Control With Distributed Delay

An artificial Earth satellite (AES) with three different principal central moments of inertia is under consideration. The AES moves along a Keplerian circular equatorial near-Earth orbit. The AES is equipped with electrodynamic attitude control system that simultaneously generates Lorentz and magnet...

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Bibliographic Details
Main Authors: Alexander Aleksandrov, Alexey A. Tikhonov
Format: Article
Language:English
Published: IEEE 2021-01-01
Series:IEEE Access
Subjects:
Asymptotic stability
attitude control
delay systems
electric variables control
low earth orbit satellites
magnetic variables control
Online Access:https://ieeexplore.ieee.org/document/9547264/

Internet

https://ieeexplore.ieee.org/document/9547264/

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