Attitude control of a sun-pointing spinning spacecraft by means of solar radiation pressure
Author:
Affiliation:
1. American Science and Engineering Inc., Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29939
Reference15 articles.
1. Stabilization and Attitude Control of Satellite Vehicles
2. Hilbard, R. R. "Attitude Stabilization Using Focused Radiation Pressure/' ARS Journal, Vol.31, 1961, pp.844-845.
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