Exploring the potential of fractionated spacecraft for enhanced satellite connectivity: Application to the satellite-to-cell case
MA Alandihallaj, AM Hein - Acta Astronautica, 2024 - Elsevier
This paper presents a mission concept designed for satellite-to-cell connectivity through a
fractionated CubeSat approach, aiming to fulfill the objectives set by the BlueWalker-3 …
fractionated CubeSat approach, aiming to fulfill the objectives set by the BlueWalker-3 …
Adaptive sliding mode control of tethered satellite deployment with input limitation
Z Ma, G Sun - Acta Astronautica, 2016 - Elsevier
This paper proposes a novel adaptive sliding mode tension control method for the
deployment of tethered satellite, where the input tension limitation is taken into account. The …
deployment of tethered satellite, where the input tension limitation is taken into account. The …
Constrained fuel-free control for spacecraft electromagnetic docking in elliptical orbits
K Shi, C Liu, Z Sun - Acta Astronautica, 2019 - Elsevier
This paper addresses the control problem of spacecraft electromagnetic docking in the
presence of external disturbances, fault signals, elliptical eccentricity, and input magnitude …
presence of external disturbances, fault signals, elliptical eccentricity, and input magnitude …
Stable cargo transportation for underactuated partial space elevator with model uncertainties and disturbances
T He, Z Zhu, J Luo - Advances in Space Research, 2024 - Elsevier
An adaptive neural network energy-based control approach is proposed in this paper to
address the issue of stabilizing a partial space elevator during cargo transportation. The …
address the issue of stabilizing a partial space elevator during cargo transportation. The …
Fuel-Efficient and Fault-Tolerant CubeSat Orbit Correction via Machine Learning-Based Adaptive Control.
M Ramezani, M Alandihallaj… - Aerospace (MDPI …, 2024 - search.ebscohost.com
The increasing deployment of CubeSats in space missions necessitates the development of
efficient and reliable orbital maneuvering techniques, particularly given the constraints on …
efficient and reliable orbital maneuvering techniques, particularly given the constraints on …
Adaptive hierarchical sliding mode control with input saturation for attitude regulation of multi-satellite tethered system
Z Ma, G Sun - The Journal of the Astronautical Sciences, 2017 - Springer
This paper proposes a novel adaptive hierarchical sliding mode control for the attitude
regulation of the multi-satellite inline tethered system, where the input saturation is taken into …
regulation of the multi-satellite inline tethered system, where the input saturation is taken into …
Multiple-horizon multiple-model predictive control of electromagnetic tethered satellite system
MA AlandiHallaj, N Assadian - Acta Astronautica, 2019 - Elsevier
This study aims to investigate the control of the electromagnetic tethered satellite system
using a Model Predictive Control (MPC) scheme. The electromagnetic tethered satellite …
using a Model Predictive Control (MPC) scheme. The electromagnetic tethered satellite …
Sliding mode control of electromagnetic tethered satellite formation
MAA Hallaj, N Assadian - Advances in space research, 2016 - Elsevier
This paper investigates the control of tethered satellite formation actuated by
electromagnetic dipoles and reaction wheels using the robust sliding mode control …
electromagnetic dipoles and reaction wheels using the robust sliding mode control …
Improved sliding mode tracking control for spacecraft electromagnetic separation supporting on-orbit assembly
C Liu, Y Ma, X Yue, K Shi - Advances in Space Research, 2024 - Elsevier
This paper addresses the electromagnetic separation problem for mass-unknown spacecraft
in elliptical orbits that play a significant role in on-orbit assembly and other future space …
in elliptical orbits that play a significant role in on-orbit assembly and other future space …
Null motion strategy for spacecraft large angle agile maneuvering using hybrid actuators
Abstract Control Moment Gyro (CMG) and Reaction Wheel (RW) generally serve in different
spacecraft control tasks due to their unique characteristics, such as large output torque and …
spacecraft control tasks due to their unique characteristics, such as large output torque and …