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Some space missions, such as the removal of space debris and the maintenance of nonfunctional satellites by spacecrafts, make some parameters uncertain. We present an approach to estimate their real values during a normal mission of operation.
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This page is a summary of: Finite-Time Concurrent Learning Adaptive Control for Spacecraft with Inertia Parameter Identification, Journal of Guidance Control and Dynamics, March 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g004803.
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