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 …

An orbital-attitude coupled control framework for a full-scale flexible electric solar wind sail spacecraft in orbital transformation missions

S Zeng, W Fan, H Ren - Aerospace Science and Technology, 2024 - Elsevier
In this work, a novel orbital-attitude coupled control framework is developed for the electric
solar wind sail (E-sail) spacecraft, aiming to handle the orbital transformation and attitude …

Generalized sail trajectory approximation with applications to MagSails

M Bassetto, AA Quarta, G Mengali - Aerospace Science and Technology, 2021 - Elsevier
This paper investigates approximate solutions to the two-dimensional equations of motion of
a generalized sail-based spacecraft. A generalized sail is a propellantless propulsion …

Rapid optimization of continuous trajectory for multi-target exploration propelled by electric sails

M Huo, R **, J Qi, N Peng, L Yang, T Wang… - Aerospace Science and …, 2022 - Elsevier
As an innovative spacecraft propellantless propulsion technology, the electric sail can
generate electric fields that interact with the solar wind, generating continuous propulsive …

Rapid cooperative optimization of continuous trajectory for electric sails in multiple formation reconstruction scenarios

R **, M Huo, Y Xu, C Zhao, L Yang, N Qi - Aerospace Science and …, 2023 - Elsevier
In satellite formation missions, conventional low-thrust spacecraft need to continuously
consume fuel to maintain a stable formation configuration, which limits the mission period …

Recovery trajectory planning for the reusable launch vehicle

G Cheng, W **g, C Gao - Aerospace Science and Technology, 2021 - Elsevier
Trajectory planning method for the entire recovery process of the reusable launch vehicle is
studied. Firstly, a revised trajectory correction method (RTCM) is proposed to reduce the …

Linearized relative motion and proximity control of E-sail-based displaced orbits

X Pan, AA Quarta, G Mengali, M Xu - Aerospace Science and Technology, 2020 - Elsevier
This paper discusses the linearized relative motion and control of Electric Solar Wind Sails
(E-sails) operating in formation flight around a heliocentric displaced orbit. An E-sail is …

Attitude control and stability analysis of electric sail

C Du, ZH Zhu, J Kang - IEEE Transactions on Aerospace and …, 2022 - ieeexplore.ieee.org
This article investigates the attitude control and stability analysis of an electric solar wind sail
(E-sail) by considering elastic deflection of tethers while assuming main spacecraft and …

Design and simulation of a flexible bending actuator for solar sail attitude control

M Liu, Z Wang, D Ikeuchi, J Fu, X Wu - Aerospace, 2021 - mdpi.com
This paper presents the design of a flexible bending actuator using shape memory alloy
(SMA) and its integration in attitude control for solar sailing. The SMA actuator has …

Dynamic characterization and sail angle control of electric solar wind sail by high-fidelity tether dynamics

C Du, ZH Zhu - Acta Astronautica, 2021 - Elsevier
This paper investigates the spin rate bounds, the configuration stability subject to the solar
wind fluctuations, and sail angle control of an electric solar wind sail (E-sail) by a high …