Sunflower mission concept for high-altitude earth observation in LEO via nanosatellite with pyramidal solar sail

Author:

Berthet MaximilienORCID,Suzuki KojiroORCID

Funder

Japan Society for the Promotion of Science

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference86 articles.

1. T. Chujo, Propellant-free attitude-trajectory control of solar sails with variable shape mechanism, in: AAS/AIAA Astrodynamics Specialist Conference, Paper AAS 20-478, Virtual, 2020.

2. Propellant-free attitude control of solar sails with variable-shape mechanisms;Chujo;Acta Astronaut.,2022

3. K. Oguri, R. Funase, Time-optimal attitude control law with a strategy of applying to orbital control for spinning solar sail driven by reflectivity control, in: AAS/AIAA Space Flight Mechanics Meeting, Paper AAS 16-329, Santa Fe, 2016.

4. Y. Takao, O. Mori, S. Kikuchi, Y. Oki, A.K. Sugihara, T. Kusumoto, Constellation Around Small Bodies Using Spinning Solar Sails Under Simultaneous Orbit-Attitude-Structure Control, in: 6th International Symposium on Space Sailing, New York, USA, 2023.

5. Attitude stability and altitude control of a variable-geometry Earth-orbiting solar sail;Felicetti;J. Guid. Control Dyn.,2016

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