| Neural network-based fault diagnosis for spacecraft with single-gimbal control moment gyros |
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| 作者姓名： | Yuandong LI Qinglei HU Xiaodong SHAO |
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| 作者单位： | 1. School of Automation Science and Electrical Engineering, Beihang University;2. Beihang Hangzhou Innovation Institute Yuhang;3. School of Aeronautic Science and Engineering, Beihang University |
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| 基金项目： | supported in part by the National Natural Science Foundation of China (Nos. 61960206011, 61903018,61633003)；;the National Defense Basic Scientific Research program of China (No. JCKY2018203B022)；;Beijing Natural Science Foundation of China (No. JQ19017)；;the China Postdoctoral Science Foundation (No. 2021M690300)； |
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| 摘 要： | This paper proposes a neural network-based fault diagnosis scheme to address the problem of fault isolation and estimation for the Single-Gimbal Control Moment Gyroscopes(SGCMGs) of spacecraft in a periodic orbit. To this end, a disturbance observer based on neural network is developed for active anti-disturbance, so as to improve the accuracy of fault diagnosis.The periodic disturbance on orbit can be decoupled with fault by resorting to the fitting and memory ability of neural network. Subsequ...
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| 收稿时间： | 28 February 2021 |
Neural network-based fault diagnosis for spacecraft with single-gimbal control moment gyros |
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| Yuandong LI,Qinglei HU,Xiaodong SHAO.Neural network-based fault diagnosis for spacecraft with single-gimbal control moment gyros[J].Chinese Journal of Aeronautics,2022,35(7):261-273. |
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| Institution: | 1. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100083, China;2. Beihang Hangzhou Innovation Institute Yuhang, Hangzhou 310023, China;3. School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China |
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| Abstract: | This paper proposes a neural network-based fault diagnosis scheme to address the problem of fault isolation and estimation for the Single-Gimbal Control Moment Gyroscopes (SGCMGs) of spacecraft in a periodic orbit. To this end, a disturbance observer based on neural network is developed for active anti-disturbance, so as to improve the accuracy of fault diagnosis. The periodic disturbance on orbit can be decoupled with fault by resorting to the fitting and memory ability of neural network. Subsequently, the fault diagnosis scheme is established based on the idea of information fusion. The data of spacecraft attitude and gimbals position are combined to implement fault isolation and estimation based on adaptive estimator and neural network. Then, an adaptive sliding mode controller incorporating the disturbance and fault estimation results is designed to achieve active fault-tolerant control. In addition, the paper gives the proof of the stability of the proposed schemes, and the simulation results show that the proposed scheme achieves better diagnosis and control results than compared algorithm. |
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| Keywords: | Control moment gyro Fault diagnosis Fault-tolerant control Neural networks Spacecraft attitude control |
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