An optimal steering law has been developed for meeting the requirements of maximizing the apse-line precession capability and the solar rotation required to attain a precession rate for GeoSail mission. The steering law takes into account all of the fundamental effects influencing the sail performance capabilities, including the shadowing effects due to the eclipse periods. A linear relationship obtained between the solar sail characteristic acceleration and the apse-line precession rate, allow evaluation of solar sail acceleration, ae necessary to perform the mission. The value of solar sail acceleration can be increased by a safety margin to compensate for the optical characteristic degradation of the sail due to a long residence in a hos...
The concept of using a solar sail for the repositioning maneuver of a spacecraft on a heliocentric o...
With increased interest in solar sailing from both ESA and NASA for future science missions comes th...
International audienceThe aim of this paper is to analyze the optimal trajectories of a spacecraft s...
An optimal steering law for sails that exploit both solar and infrared planetary radiation pressure ...
Solar sailing is a spacecraft propulsion method relying solely on solar radiation pressure to provid...
This paper analyzes the problem of finding the optimal steering law for a flat solar sail whose prop...
Solar sailing is a spacecraft propulsion method relying solely on solar radiation pressure to provid...
The direction and magnitude of a solar sail acceleration are strongly related. For this reason, once...
A simplified solar sail steering law is discussed in which the sail clock angle is used as the only ...
The aim of this paper is to devise a local optimal strategy for orbital inclination change of solar ...
The aim of this paper is to devise a local optimal strategy for the orbital inclination change of so...
The optimization of a solar sail-based orbital transfer amounts to searching for the control law tha...
Abstract: The geocentric boost of SCSS with a flat solar sail, which is a mirror reflector...
The aim of this paper is to analyze optimal trajectories of a solar sail-based spacecraft in mission...
The concept of using a solar sail for the repositioning maneuver of a spacecraft on a heliocentric o...
With increased interest in solar sailing from both ESA and NASA for future science missions comes th...
International audienceThe aim of this paper is to analyze the optimal trajectories of a spacecraft s...
An optimal steering law for sails that exploit both solar and infrared planetary radiation pressure ...
Solar sailing is a spacecraft propulsion method relying solely on solar radiation pressure to provid...
This paper analyzes the problem of finding the optimal steering law for a flat solar sail whose prop...
Solar sailing is a spacecraft propulsion method relying solely on solar radiation pressure to provid...
The direction and magnitude of a solar sail acceleration are strongly related. For this reason, once...
A simplified solar sail steering law is discussed in which the sail clock angle is used as the only ...
The aim of this paper is to devise a local optimal strategy for orbital inclination change of solar ...
The aim of this paper is to devise a local optimal strategy for the orbital inclination change of so...
The optimization of a solar sail-based orbital transfer amounts to searching for the control law tha...
Abstract: The geocentric boost of SCSS with a flat solar sail, which is a mirror reflector...
The aim of this paper is to analyze optimal trajectories of a solar sail-based spacecraft in mission...
The concept of using a solar sail for the repositioning maneuver of a spacecraft on a heliocentric o...
With increased interest in solar sailing from both ESA and NASA for future science missions comes th...
International audienceThe aim of this paper is to analyze the optimal trajectories of a spacecraft s...