Spiral trajectories induced by radial thrust with applications to generalized sails

M Bassetto, AA Quarta, G Mengali, V Cipolla - Astrodynamics, 2021 - Springer
In this study, new analytical solutions to the equations of motion of a propelled spacecraft
are investigated using a shape-based approach. There is an assumption that the spacecraft …

Warm start for low-thrust trajectory optimization via switched system

D Wu, F Jiang, J Li - Journal of Guidance, Control, and Dynamics, 2021 - arc.aiaa.org
OVER the past few decades, low-thrust propulsion systems have attracted great attention
due to their high specific impulse, allowing reductions in propellant consumption [1]. To seek …

Solar sail optimal transfer between heliostationary points

AA Quarta, G Mengali, L Niccolai - Journal of Guidance, Control, and …, 2020 - arc.aiaa.org
A NOTABLE feature of propellantless propulsion systems such as solar sails [1, 2] is their
capability to generate a continuous thrust for a long time span, theoretically limited only by …

Smart dust option for geomagnetic tail exploration

AA Quarta, G Mengali, L Niccolai - Astrodynamics, 2019 - Springer
In-situ measurements are necessary for a long-term analysis of the spatial structure of the
geomagnetic tail. This type of mission requires the use of a propellantless propulsion …

Analytical solution to logarithmic spiral trajectories with circumferential thrust and mission applications

M Bassetto, AA Quarta, G Mengali - Astrodynamics, 2022 - Springer
This study made use of a shape-based method to analyze the orbital dynamics of a
spacecraft subject to a continuous propulsive acceleration acting along the circumferential …

Optimal control of rapid cooperative spacecraft rendezvous with multiple specific-direction thrusts

P Su, W Feng, Y Kun, Z Junfeng - Proceedings of the …, 2020 - journals.sagepub.com
Focusing on the long-distance rapid cooperative rendezvous of two spacecraft under finite
continuous thrust, this paper proposes a practical strategy for space operation using multiple …

Solar sail optimal maneuvers for heliocentric orbit apse line rotation

AA Quarta, G Mengali, L Niccolai, C Bianchi - Acta Astronautica, 2022 - Elsevier
The aim of this work is to investigate the performance of a solar sail-based spacecraft in an
optimal apse line rotation maneuver. Considering a heliocentric two-body motion and a low …