Nonlinear Momentum Transfer Control of Spacecraft by Feedback Linearization
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Daejon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3909
Reference16 articles.
1. Kaplan, M., Modern Spacecraft Dynamics and Control, 1st ed.Wiley, New York, 1976, pp.367-379.
2. Perturbation Solution for the Flat Spin Recovery of a Dual-§pin Spacecraft
3. Spacecraft large angle rotational maneuvers with optimal momentum transfer
4. Junkins, J. L., and Turner, J. D., Optimal Spacecraft Rotational Maneuvers, 1st ed.Elsevier, Amsterdam, 1986, pp.267-287.
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