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This paper presents a composite adaptive control system for the orbit and hovering control of a spacecraft in the vicinity of rotating asteroids. The composite identifier with a regressor integral excitation term achieves parameter error convergence.
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This page is a summary of: Composite Adaptive Orbit Control and Parameter Estimation by Integral Excitation Around Asteroids, Journal of Guidance Control and Dynamics, September 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007270.
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