Abstract
Control Moment Gyroscopes (CMGs) are usually used as the actuator for large spacecraft due to their torque amplification characteristics. For example, the International Space Station (ISS) launched in 1998, and the Tianhe core module launched in 2021 are all equipped with CMGs. Compared with other momentum exchange devices like reaction wheels, the structure and working principle of CMGs are more complex. In practical applications, CMGs are prone to various types of faults and are difficult to implement fault diagnosis.
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Hu, Q., Shao, X., Guo, L. (2023). Intelligent Fault Diagnosis and Fault-Tolerant Control of Spacecraft. In: Intelligent Autonomous Control of Spacecraft with Multiple Constraints. Springer, Singapore. https://doi.org/10.1007/978-981-99-0681-9_5
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DOI: https://doi.org/10.1007/978-981-99-0681-9_5
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