Abstract
The spinning deployment process of solar sails is analyzed in this study. A simplified model is established by considering the out-of-plane and in-plane motions of solar sails. The influences of structure parameters, initial conditions, and feedback control parameters are also analyzed. A method to build the geometric model of a solar sail is presented by analyzing the folding process of solar sails. The finite element model of solar sails is then established, which contains continuous cables and sail membranes. The dynamics of the second-stage deployment of solar sails are simulated by using ABAQUS software. The influences of the rotational speed and out-of-plane movement of the hub are analyzed by different tip masses, initial velocities, and control parameters. Compared with the results from theoretical models, simulation results show good agreements.
Original language | English |
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Pages (from-to) | 1719-1728 |
Number of pages | 10 |
Journal | Chinese Journal of Aeronautics |
Volume | 30 |
Issue number | 5 |
DOIs | |
Publication status | Published - Oct 2017 |
Keywords
- Deployment
- Dynamics
- Solar sail
- Spinning
- Stability