A review of Smart Dust architecture, dynamics, and mission applications

L Niccolai, M Bassetto, AA Quarta, G Mengali - Progress in Aerospace …, 2019 - Elsevier
A Smart Dust is a propellantless femtosatellite, with a characteristic side length of a few
millimeters and a high value of its area-to-mass ratio. It exploits the solar radiation pressure …

Collinear artificial equilibrium point maintenance with a wrinkled solar sail

C Bianchi, L Niccolai, G Mengali, AA Quarta - Aerospace Science and …, 2021 - Elsevier
Propellantless propulsion systems allow innovative mission scenarios to be envisaged,
including the generation and the stabilization of artificial equilibrium points in the circular …

Near earth asteroid scout thrust and torque model

A Heaton, N Ahmad, K Miller - International Symposium on Solar …, 2017 - ntrs.nasa.gov
The Near Earth Asteroid (NEA) Scout is a solar sail mission whose objective is to scout at
least one Near Earth Asteroid in preparation for manned missions to asteroids. NEA Scout …

Feedback control law of solar sail with variable surface reflectivity at Sun-Earth collinear equilibrium points

L Niccolai, G Mengali, AA Quarta, A Caruso - Aerospace Science and …, 2020 - Elsevier
A solar sail generates thrust without consuming any propellant, so it constitutes a promising
option for mission scenarios requiring a continuous propulsive acceleration, such as the …

LightSail 2 solar sail control and orbit evolution

JR Mansell, JM Bellardo, B Betts, B Plante, DA Spencer - Aerospace, 2023 - mdpi.com
The propellantless thrust of solar sails makes them capable of entirely new classes of
missions compared to conventional or electric engines. Initiated in 2010, the Planetary …

Road Map to L4/L5 with a solar sail

A Farrés, J Heiligers, N Miguel - Aerospace Science and Technology, 2019 - Elsevier
This paper explores the capability of solar sails to transfer a probe from the displaced Sun-
Earth L 1 and L 2 libration points to the region of practical stability (RPS) around the …

Analytical solution of the optimal steering law for non-ideal solar sail

L Niccolai, AA Quarta, G Mengali - Aerospace Science and Technology, 2017 - Elsevier
This paper analyzes the problem of finding the optimal steering law for a flat solar sail whose
propulsive acceleration is described by an optical force model. In particular, the problem …

Comparison between direct and indirect approach to solar sail circle-to-circle orbit raising optimization

A Caruso, AA Quarta, G Mengali - Astrodynamics, 2019 - Springer
This paper deals with the optimization of the transfer trajectory of a solar sail-based
spacecraft between circular and coplanar heliocentric orbits. The problem is addressed …

[HTML][HTML] Deorbiting spacecraft with passively stabilised attitude using a simplified quasi-rhombic-pyramid sail

N Miguel, C Colombo - Advances in Space Research, 2021 - Elsevier
This paper studies deorbiting using an analogue to the quasi-rhombic-pyramid concept for
planar motion. The focus is on maintaining a stable (meaning oscillatory) attitude close to …

Modular Dynamic Modeling and Simulation of a Cable-Actuated Flexible Solar Sail

KR Bunker, R Caverly - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
This paper presents a modular dynamic modeling approach to simulate a solar sail
embedded with actuated cables within its flexible structure. The cables are routed along the …