Detumbling Attitude Control Analysis Considering an Electrostatic Pusher Configuration
Author:
Affiliation:
1. Samara National Research University, Samara, 443086, Russian
2. University of Colorado, Boulder, Colorado 80309-0431
Funder
Russian Foundation for Basic Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G003966
Reference22 articles.
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5. Geosynchronous Large Debris Reorbiter: Challenges and Prospects
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