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 …
research is quite broad and multi-disciplinary; this paper focuses mainly on areas such as …
Review on solar sail technology
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 …
dynamics. Within the area of orbital dynamics, methods relevant to transfer trajectory design …
Survey of highly non-Keplerian orbits with low-thrust propulsion
CELESTIAL mechanics has traditionally been concerned with orbital motion under the
action of a conservative gravitational potential. In particular, the inverse square gravitational …
action of a conservative gravitational potential. In particular, the inverse square gravitational …
Solar sail body-fixed hovering over elongated asteroids
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 …
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 …
(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
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 …
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 …
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 …
for decades because its optical characteristics can be altered by electrical excitation. The …
Solar sail cooperative formation flying around L2-type artificial equilibrium points
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] …
formation, flying around an L 2-type artificial equilibrium point in the Sun-[Earth+ Moon] …
Non-Keplerian orbits for electric sails
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 …
be otherwise unfeasible through conventional propulsion systems. In particular, the aim of …