Coordinated control of high-order fully actuated multiagent systems and its application: A predictive control strategy

DW Zhang, GP Liu, L Cao - IEEE/ASME Transactions on …, 2022 - ieeexplore.ieee.org
This research is devoted to the coordinated control of high-order fully actuated multiagent
systems (HOFA-MASs). A predictive control strategy is developed to realize the coordination …

[HTML][HTML] Experimental verification and comparison of fuzzy and PID controllers for attitude control of nanosatellites

A Bello, KS Olfe, J Rodríguez, JM Ezquerro… - Advances in Space …, 2023 - Elsevier
Modern control algorithms based on artificial intelligence have shown good results in many
application fields. That is why some researchers have made an effort to introduce them in …

Attitude control experiment of a spinning spacecraft using only magnetic torquers

K Kimura, Y Shoji, S Satoh, K Yamada - Advances in Space Research, 2023 - Elsevier
Magnetic torquers are attitude control devices used in spacecraft systems, and extensive
research has been conducted on the attitude control of such spacecraft systems equipped …

Implementation and hardware-in-the-loop simulation of a magnetic detumbling and pointing control based on three-axis magnetometer data

MS Farissi, S Carletta, A Nascetti, P Teofilatto - Aerospace, 2019 - mdpi.com
The subject of this work is the implementation and experimental testing of a purely magnetic
attitude control strategy, which can provide stabilization after the deployment and pointing of …

Extended validation of a ground-based three-axis spacecraft simulator model

HS Ousaloo, G Sharifi… - Proceedings of the …, 2021 - journals.sagepub.com
The ground-based spacecraft dynamics simulator plays an important role in the
implementation and validation of attitude control scenarios before a mission. The …

Globally asymptotic three-axis attitude control for a two-wheeled small satellite

HS Ousaloo - Acta Astronautica, 2019 - Elsevier
This paper focuses on investigating and analyzing hybrid control strategies of onboard
magnetic torque bars (MTs) and reaction wheels (RWs) for attitude stabilization on three …

A high-order disturbance nutation/wobble control for unbalanced spinning satellites

HS Ousaloo, B Akbarinia - Advances in Space Research, 2024 - Elsevier
This paper introduces a novel active nutation/wobble rejection control method for spinning
satellites enduring thrusting disturbances and reaction wheel limitations. Our approach …

Mass properties identification and automatic mass balancing system for satellite attitude dynamics simulator

G Sharifi, M Mirshams… - Proceedings of the …, 2019 - journals.sagepub.com
A Satellite Attitude Dynamics Simulator is a low-cost, ground-based system made to
simulate the conditions of a weightless satellite in space. The identification of the mass …

Spin Axis Control Using Reaction Wheels: Modeling and Experimental Validation

HS Ousaloo, B Akbarinia - Journal of Aerospace Engineering, 2022 - ascelibrary.org
This paper focuses on a single-axis control of a wheeled spin satellite while the entire
angular momentum is not zero. The presented technique includes a feedback control law …

[PDF][PDF] A Review Paper: The Dynamics, Kinematics, Design and Control of Satellite Simulators with Spherical Air Bearing

R Yeşilay, A Ankaralı, MA Afşar - Global Conference on …, 2021 - researchgate.net
Because of the high cost and the long-life requirements of the satellites, they are subjected
to various tests on ground before launching. So that all the units assembled to the satellite …