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Published in 2017 at "Nonlinear Dynamics"
DOI: 10.1007/s11071-017-3762-0
Abstract: The attitude dynamics and control for solar sail orbiting a celestial body (e.g., the Earth) are critical for the space missions. In the paper, the pitch dynamics is addressed by considering the torques by the…
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Keywords:
pitch;
pitch dynamics;
motion;
solar sail ... See more keywords
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Published in 2020 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2019.10.028
Abstract: Abstract The aim of this paper is to propose a distributed control architecture for a solar sail-based formation, flying around an L 2 -type artificial equilibrium point in the Sun-[Earth + Moon] circular restricted three-body problem. Two…
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Keywords:
formation flying;
solar sail;
formation;
flying around ... See more keywords
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Published in 2020 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2020.07.010
Abstract: Abstract The aim of this paper is to evaluate the effect of a maximum admissible value of the sail cone angle on the transfer performance of a solar sail-based spacecraft in an interplanetary mission scenario.…
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Keywords:
attitude constraints;
solar sail;
sail;
effects attitude ... See more keywords
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Published in 2021 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2021.04.011
Abstract: Abstract This paper presents a planetary elliptic displaced orbit (PEDO) for a solar sail with reflectivity control devices (RCDs). The problem of multiple solar sail formation flying in which the leader follows the PEDO is…
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Keywords:
sail;
control;
solar sail;
multiple solar ... See more keywords
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Published in 2017 at "Advances in Space Research"
DOI: 10.1016/j.asr.2016.11.020
Abstract: Abstract Solar Radiation Pressure (SRP) and albedo effects are investigated in the circular restricted three-body problem for a system consisting of the Sun, a reflective minor body and a solar sail. As an approximation of…
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Keywords:
solar sail;
radiation pressure;
body;
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Published in 2019 at "Advances in Space Research"
DOI: 10.1016/j.asr.2019.11.037
Abstract: Abstract The heliocentric orbital dynamics of a spacecraft propelled by a solar sail is affected by some uncertainty sources, including possible inaccuracies in the measurement of the sail film optical properties. Moreover, the solar radiation…
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Keywords:
parameter measurement;
optical parameter;
measurement uncertainties;
solar sail ... See more keywords
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Published in 2020 at "Advances in Space Research"
DOI: 10.1016/j.asr.2020.01.020
Abstract: Abstract In this paper, we present an analysis of effect of wrinkles on the solar sail performance. We describe different analytical, semi-analytical and numerical approaches to the calculation of general large-scale curvature of a solar…
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Keywords:
generalized sail;
solar sail;
sail;
model solar ... See more keywords
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Published in 2020 at "Advances in Space Research"
DOI: 10.1016/j.asr.2020.06.017
Abstract: Abstract Detailed dynamic modelling of a solar sail requires recording of solar radiation pressure influence. A photon-solar sail is determined by the thrust value and the direction. We define the solar sail’s reflectivity depending on…
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Keywords:
parameters solar;
solar sail;
optical parameters;
sail ... See more keywords
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Published in 2020 at "Advances in Space Research"
DOI: 10.1016/j.asr.2020.10.001
Abstract: Abstract For precursor solar sail activities a strategy for a controlled deployment of large membranes was developed based on a combination of zig-zag folding and coiling of triangular sail segments spanned between crossed booms. This…
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Keywords:
deployment;
solar sail;
sail;
performance ... See more keywords
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2
Published in 2022 at "IEEE Transactions on Aerospace and Electronic Systems"
DOI: 10.1109/taes.2022.3151588
Abstract: Solar sail appears to be promising and effective spacecraft in interplanetary missions; however, performance degradation is inevitable during its long-term voyage, caused by materials wastage and accidents. This study designed a solar sail with numerous…
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Keywords:
numerous discrete;
sail numerous;
control;
discrete elements ... See more keywords
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Published in 2019 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/0954410018764183
Abstract: A finite element approach is used to calculate the components of forces and moments acting on a square solar sail at a sun-sail distance equal to one astronomical unit. The model takes into account the…
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Keywords:
finite element;
analysis;
solar sail;
sail ... See more keywords