Kinematic accuracy reliability evaluation method of space deployable mechanism based on dynamic model
Space deployable mechanisms are widely used in aerospace missions. The uncertainties in the geometric or physical parameters seriously affect the kinematic accuracy of the mechanism during the deployment process. In this paper, a kinematic accuracy reliability evaluation method of the space deployab...
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Published in | Journal of physics. Conference series Vol. 2762; no. 1; pp. 012010 - 12018 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
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Bristol
IOP Publishing
01.05.2024
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Abstract | Space deployable mechanisms are widely used in aerospace missions. The uncertainties in the geometric or physical parameters seriously affect the kinematic accuracy of the mechanism during the deployment process. In this paper, a kinematic accuracy reliability evaluation method of the space deployable mechanism based on dynamic model and adaptive hybrid surrogate models is presented. Firstly, the dynamic model of the space deployable mechanism is established based on the Lagrange method, and the motion error function considering the factors such as the mass, dimension and load is established. In order to improve the efficiency, an adaptive hybrid surrogate model reliability evaluation method based on improved weight measurement method is further proposed. The weight measurement method considers the global errors and local errors of the models. Finally, the Monte Carlo method is used to verify the accuracy of the hybrid surrogate model method. The relative error of the failure probability calculated by the proposed method is within 2.5 %, indicating that the proposed method has high calculation accuracy and efficiency. |
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AbstractList | Space deployable mechanisms are widely used in aerospace missions. The uncertainties in the geometric or physical parameters seriously affect the kinematic accuracy of the mechanism during the deployment process. In this paper, a kinematic accuracy reliability evaluation method of the space deployable mechanism based on dynamic model and adaptive hybrid surrogate models is presented. Firstly, the dynamic model of the space deployable mechanism is established based on the Lagrange method, and the motion error function considering the factors such as the mass, dimension and load is established. In order to improve the efficiency, an adaptive hybrid surrogate model reliability evaluation method based on improved weight measurement method is further proposed. The weight measurement method considers the global errors and local errors of the models. Finally, the Monte Carlo method is used to verify the accuracy of the hybrid surrogate model method. The relative error of the failure probability calculated by the proposed method is within 2.5 %, indicating that the proposed method has high calculation accuracy and efficiency. |
Author | Zhuang, Xinchen Sun, Zhongchao Liu, Chang Yu, Tianxiang |
Author_xml | – sequence: 1 givenname: Chang surname: Liu fullname: Liu, Chang organization: School of Aeronautics, Northwestern Polytechnical University , China – sequence: 2 givenname: Xinchen surname: Zhuang fullname: Zhuang, Xinchen organization: School of Aeronautics, Northwestern Polytechnical University , China – sequence: 3 givenname: Zhongchao surname: Sun fullname: Sun, Zhongchao organization: School of Aeronautics, Northwestern Polytechnical University , China – sequence: 4 givenname: Tianxiang surname: Yu fullname: Yu, Tianxiang organization: School of Aeronautics, Northwestern Polytechnical University , China |
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SubjectTerms | Accuracy Deployable mechanism Dynamic models Error functions Hybrid surrogate model Kinematic accuracy Kinematics Measurement methods Monte Carlo simulation Physical properties Reliability analysis Reliability evaluation method Weight measurement |
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Title | Kinematic accuracy reliability evaluation method of space deployable mechanism based on dynamic model |
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