Liquid Crystal Device with Reflective Microstructure for Attitude Control
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Kanagawa 252-5210, Japan
2. The University of Tokyo, Tokyo 113-8654, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34165
Reference9 articles.
1. Hayabusa2 Mission Overview
2. Generalized Attitude Model for Momentum-Biased Solar Sail Spacecraft
3. IKAROS and Extended Solar Power Sail Missions for Outer Planetary Exploration
4. Achievement of IKAROS — Japanese deep space solar sail demonstration mission
5. On-orbit verification of fuel-free attitude control system for spinning solar sail utilizing solar radiation pressure
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