Solar sail technology—A state of the art review

B Fu, E Sperber, F Eke - Progress in Aerospace Sciences, 2016 - Elsevier
In this paper, the current state of the art of solar sail technology is reviewed. Solar sail
research is quite broad and multi-disciplinary; this paper focuses mainly on areas such as …

Review on solar sail technology

S Gong, M Macdonald - Astrodynamics, 2019 - Springer
This paper reviews solar sail trajectory design and dynamics, attitude control, and structural
dynamics. Within the area of orbital dynamics, methods relevant to transfer trajectory design …

Survey of highly non-Keplerian orbits with low-thrust propulsion

RJ McKay, M Macdonald, J Biggs… - Journal of Guidance …, 2011 - arc.aiaa.org
CELESTIAL mechanics has traditionally been concerned with orbital motion under the
action of a conservative gravitational potential. In particular, the inverse square gravitational …

Solar sail body-fixed hovering over elongated asteroids

X Zeng, S Gong, J Li, KT Alfriend - Journal of Guidance, Control, and …, 2016 - arc.aiaa.org
Solar sail spacecraft are proposed to accomplish body-fixed hovering missions over
elongated asteroids. The body-fixed hovering flight is to maintain a fixed position relative to …

Periodic orbits above the ecliptic in the solar-sail restricted three-body problem

TJ Waters, CR McInnes - Journal of Guidance, Control, and Dynamics, 2007 - arc.aiaa.org
We consider periodic orbits in the circular restricted three-body problem, where the third
(small) body is a solar sail. In particular, we consider orbits about equilibrium points in the …

Study on the connection between the rotating mass dipole and natural elongated bodies

X Zeng, F Jiang, J Li, H Baoyin - Astrophysics and Space Science, 2015 - Springer
The focus of this paper is to connect the rotating mass dipole with natural elongated bodies.
The dipole system is consisted with two point masses connected with a massless rod in a …

Sunjammer: Preliminary end-to-end mission design

J Heiligers, B Diedrich, W Derbes… - AIAA/AAS astrodynamics …, 2014 - arc.aiaa.org
This paper provides a preliminary end-to-end mission design for NASA's Sunjammer solar
sail mission, which is scheduled for ground test deployment in 2015 with launch at a later …

Coupled control of reflectivity modulated solar sail for GeoSail formation flying

J Mu, S Gong, J Li - Journal of Guidance, Control, and Dynamics, 2015 - arc.aiaa.org
The use of the electrochromic device has been proposed for the attitude control of spacecraft
for decades because its optical characteristics can be altered by electrical excitation. The …

Solar sail cooperative formation flying around L2-type artificial equilibrium points

W Wang, H Baoyin, G Mengali, AA Quarta - Acta Astronautica, 2020 - Elsevier
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] …

Non-Keplerian orbits for electric sails

G Mengali, AA Quarta - Celestial Mechanics and Dynamical Astronomy, 2009 - Springer
An electric sail is capable of guaranteeing the fulfilment of a class of trajectories that would
be otherwise unfeasible through conventional propulsion systems. In particular, the aim of …