Stability of Spinning Solar Sail-craft Containing A Huge Membrane

Author:

Nakano Tomoki1,Mori Osamu2,Kawaguchi Jun'ichiro2

Affiliation:

1. University of Tokyo

2. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Reference6 articles.

1. D.Murphy, T.Trautt, M.McEachen, D.Meaaner, G.Laue, P.Gierow "Progress and Plans for System Demonstration of a Scalable Square Solar Sail,"14thASS/AIAASpaceFlightMechanicsConference

2. Design Study of a Square Solar Sail Architecture

3. Geometric Imperfection Effects in an Elastically Deployable Isogrid Column

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1. Numerical Analysis on Optimal Deployment Configuration of Tightly-Folded Device-Laden Space Membrane;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2022

2. Computational Multibody Dynamics of Heliogyro Solar Sail under Spin-Deployment;AIAA Scitech 2020 Forum;2020-01-05

3. Stability Analysis of Generalized Sail Dynamics Model;Journal of Guidance, Control, and Dynamics;2018-09

4. Interplanetary Mission Design for Spinning Solar Sails Utilizing Active Shape Control of Sail Membranes;2018 Space Flight Mechanics Meeting;2018-01-07

5. Active Shape Control of Spinning Membrane Space Structures and Its Application to Solar Sailing;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2018

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