航天服软关节单历程阻力矩的数学模型
作者:
作者单位:

1.国防科技大学 空天科学学院, 湖南 长沙 410073 ;2.国防科技大学 空天任务智能规划与仿真湖南省重点实验室, 湖南 长沙 410073

作者简介:

董长林(1998—),男,吉林吉林人,博士研究生,E-mail:dcl15651075186nudt@163.com

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中图分类号:

V45

基金项目:

湖南省研究生教育创新工程和专业能力提升工程资助项目(CX20200083)


Mathematical model for single-course resistance torque of spacesuit soft joints
Author:
Affiliation:

1.College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073 , China ; 2.Hunan Key Laboratory of Intelligent Planning and Simulation for Aerospace Missions, NationalUniversity of Defense Technology, Changsha 410073 , China

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    摘要:

    针对航天服软关节单历程阻力矩的现有模型精度低、形状误差大等问题,建立了一种改进的B-W(Bouc-Wen)数学模型。通过分析航天服软关节单历程阻力矩迟滞曲线特性,引入了B-W迟滞模型,并改进以消除模型的冗余度和对称性,用于对软关节单历程阻力矩的数学表征;借鉴模拟退火算法中概率思想对多岛遗传算法中个体遗传进行操作,实现对改进B-W模型的参数进行高精度、高效率地辨识。经过航天服不同软关节仿真和实验的验证,改进后的B-W模型较现有J-A(Jiles-Atherton)模型更适用于航天服软关节单历程阻力矩的数学表征,其阻力矩方差较J-A模型降低2个数量级。结果表明,该数学模型应用于航天服软关节单历程阻力矩具有较高的精度,且对航天服不同软关节均具有较强的适用性。

    Abstract:

    Aiming at the problems of low accuracy and large shape error of existing models for single-course resistance torque of spacesuit soft joints, an improved B-W(Bouc-Wen) mathematical model was established. By analyzing the hysteresis curve characteristics of single-course resistance torque of spacesuit soft joints, the B-W hysteresis model was introduced and improved to eliminate the redundancy and symmetry of the model, which was used to characterize single-course resistance torque of soft joints mathematically. The individual genetic process of multi-island genetic algorithm was operated by using the probability thought of simulated annealing algorithm to identify the parameters of improved B-W model with high accuracy and efficiency. Based on the verification of experiments and simulations of different soft joints of spacesuit, the improved B-W model compared with the J-A(Jiles-Atherton) model is more suitable for the mathematical characterization of single-course resistance torque of spacesuit soft joints. The variance of resistance torque of improved B-W model is two orders of magnitude lower than that of J-A model. It shows that the mathematical model has high accuracy when applied to single-course resistance torque of spacesuit soft joints, and has strong applicability to different soft joints of spacesuit.

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董长林, 周仕明, 李道奎. 航天服软关节单历程阻力矩的数学模型[J]. 国防科技大学学报, 2025, 47(5): 157-164.

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  • 收稿日期:2024-05-19
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  • 在线发布日期: 2025-10-08
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