A comprehensive review of Electric Solar Wind Sail concept and its applications

M Bassetto, L Niccolai, AA Quarta, G Mengali - Progress in Aerospace …, 2022 - Elsevier
Abstract The Electric Solar Wind Sail (E-sail) is an innovative propellantless propulsion
system conceived by Pekka Janhunen in 2004 for use in interplanetary space. An E-sail …

Fractional-order fuzzy sliding mode control for the deployment of tethered satellite system under input saturation

S Xu, G Sun, Z Ma, X Li - IEEE transactions on aerospace and …, 2018 - ieeexplore.ieee.org
In this paper, a novel fractional-order fuzzy sliding mode control strategy is developed to
realize the deployment of the tethered satellite system (TSS) with input saturation. The …

Timeline Club: An optimization algorithm for solving multiple debris removal missions of the time-dependent traveling salesman problem model

N Zhang, Z Zhang, H Baoyin - Astrodynamics, 2022 - Springer
With the increase of space debris, space debris removal has gradually become a major
issue to address by worldwide space agencies. Multiple debris removal missions, in which …

A code for the analysis of missions with electrodynamic tethers

G Sánchez-Arriaga, G Borderes-Motta, L Chiabó - Acta Astronautica, 2022 - Elsevier
The main novelties and capabilities of the second version of the Bare Electrodynamic Tether
Mission Analysis Software (BETsMA v2. 0) are presented. Recent advances on Orbital …

Optimal control of nanosatellite fast deorbit using electrodynamic tether

R Zhong, ZH Zhu - Journal of Guidance, Control, and Dynamics, 2014 - arc.aiaa.org
This paper proposes a piecewise two-phased optimal control scheme for fast nanosatellite
deorbit by a short electrodynamic tether. The first phase concerns the open-loop control …

Deep learning for deorbiting control of an electrodynamic tether system

X Ma, H Wen - Acta Astronautica, 2023 - Elsevier
This paper studies the nonlinear dynamics and deorbiting control of an electrodynamic
tether (EDT) system in elliptical orbits. The orbital dynamics of the system under Lorentz …

A fuzzy control scheme for deployment of space tethered system with tension constraint

S Xu, H Wen, Z Huang, D ** - Aerospace Science and Technology, 2020 - Elsevier
This paper is concerned with fuzzy control for deployment of space tethered system subject
to tension constraint. The space tethered system under consideration consists of two …

Dynamic adaptive saturated sliding mode control for deployment of tethered satellite system

Z Ma, G Sun, Z Li - Aerospace Science and Technology, 2017 - Elsevier
This paper presents a novel adaptive dynamic sliding mode scheme for the deployment of
the tethered satellite system. To overcome the limited inputs of the dynamic model, a new …

Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration

GQ Li, ZH Zhu - Celestial Mechanics and Dynamical Astronomy, 2015 - Springer
Dynamic modeling of tethered spacecraft with the consideration of elasticity of tether is
prone to the numerical instability and error accumulation over long-term numerical …

Automatic orbital maneuver for mega-constellations maintenance with electrodynamic tethers

J Liu, G Li, ZH Zhu, M Liu, X Zhan - Aerospace Science and Technology, 2020 - Elsevier
This paper focuses on the feasibility of constellation maintenance for large-scale satellite
constellations (ie, mega-constellations) by the electrodynamic tethered multi-agent system …