Attitude Stabilization of a Satellite with Large Flexible Elements Using On-Board Actuators Only

Attitude Stabilization of a Satellite with Large Flexible Elements Using On-Board Actuators Only

Attitude control of a satellite with three flexible elements is considered. Control torque is developed by a set of reaction wheels, which are installed on the central hub of the satellite. The flexible elements are large, so the control torque constraints must be taken into account. In the paper, a...

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Bibliographic Details
Main Authors: Stepan Tkachev, Alexey Shestoperov, Anna Okhitina, Anna Nuralieva
Format: Article
Language:English
Published: MDPI AG 2023-12-01
Series:Mathematics
Subjects:
attitude control
large flexible element
linear quadratic control
asymptotic stability
particle swarm optimization
control parameter
Online Access:https://www.mdpi.com/2227-7390/11/24/4928

Internet

https://www.mdpi.com/2227-7390/11/24/4928

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