Abstract
As space missions become more and more complex, higher requirements are placed on the rapid maneuverability of spacecraft. The control moment gyros (CMGs) are more suitable for the rapid maneuvering of large-mass satellites due to the characteristic of moment amplification (Hill in J Guidance Control Dyn 39(10):2406–2418 (2016), [1]).
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Hu, Q., Shao, X., Guo, L. (2023). Reinforcement Learning-Based Dynamic Control Allocation for Spacecraft Attitude Stabilization. In: Intelligent Autonomous Control of Spacecraft with Multiple Constraints. Springer, Singapore. https://doi.org/10.1007/978-981-99-0681-9_6
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DOI: https://doi.org/10.1007/978-981-99-0681-9_6
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