电工技术学报  2023, Vol. 38 Issue (4): 1076-1087    DOI: 10.19595/j.cnki.1000-6753.tces.211217
高电压与放电 |
磁保持型航天电磁继电器性能提升与质量一致性设计
陈昊, 叶雪荣, 梁慧敏, 翟国富
哈尔滨工业大学电气工程及自动化学院 哈尔滨 150001
Performance Enhanced and Quality Consistency Design Optimization of Magnetically Latching Aerospace Electromagnetic Relay
Chen Hao, Ye Xuerong, Liang Huimin, Zhai Guofu
School of Electrical Engineering & Automation Harbin Institute of Technology Harbin 150001 China
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摘要 磁保持航天电磁继电器具有灵敏度高、发热小、功耗低、体积小等优点,广泛应用于运载火箭、卫星和空间站等航天装备,其性能与质量一致性直接影响航天装备的研发与服役进程,因此性能提升与质量一致性优化引起了广泛的关注。磁保持航天电磁继电器性能参数的计算精度和多性能互相制约下的寻优迭代效率,是影响磁保持航天电磁继电器优化效果的重要因素。该文针对最为典型、复杂的双磁钢差动式产品性能特征存在过零点、计算精度低、寻优收敛性差且效率低等特点,提出一种可适用于各类磁保持航天电磁继电器建模与迭代寻优的设计方法,即基于斯通纳-沃尔法斯模型和Preisach模型得到的非线性永磁体局部磁滞曲线,进而建立继电器虚拟样机模型,实现该继电器性能参数的准确计算。基于虚拟样机模型,使用模糊混沌展开得到代理模型的基函数,使用径向基函数方法修正实测结果与基函数计算结果之间的误差,建立性能特征代理模型,实现该磁保持航天电磁继电器性能参数的精确高效计算。在此基础上,揭示磁保持航天电磁继电器设计参数与性能特征之间的作用规律,改进差分进化算法,形成自适应最优种群迭代策略,提升寻优效率和寻优稳健性。以双磁钢差动式磁保持航天电磁继电器为例,验证所提方法的有效性。
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陈昊
叶雪荣
梁慧敏
翟国富
关键词 磁保持航天电磁继电器虚拟样机代理模型多目标寻优    
Abstract:Magnetic latching aerospace electromagnetic relay (MLAER) has high sensitivity, low heat generation, low power consumption, and small size, used in various aerospace equipment such as vehicles, spacecraft, and satellites. The calculation accuracy of MLAER performance parameters and the iterative search efficiency of the optimal combination of consistency under the constraints of multiple performance objectives are the important factors affecting the optimization of MLAER. This paper proposes a design method for modeling and iterative optimization of MLAER combined with the Stoner-Wahlfarth method and the Preisach method, based on a non-linear permanent magnet local hysteresis model. An approximate model basis function is obtained based on fuzzy chaotic expansion. The parameters of the measured prototype are determined using the fastest curvature descent, and the error between the measured and calculated values is corrected using the kriging method to achieve accurate and efficient calculation of the performance parameters of the relay. The law between the magnetic retention relay design parameter and the shape factor of the suction curve is revealed, and the differential evolution algorithm is improved to form an adaptive optimal population iteration strategy. It improves the optimization efficiency and robustness of the differential evolution algorithm in solving the magnetic retention relay optimization problem. The following results have been achieved.
(1) The magnetically maintained aerospace relay with nonlinear anisotropic permanent magnets has strong nonlinearity and the local hysteresis effect of magnetization and demagnetization. Therefore, this paper proposes a virtual prototype modeling method that can be applied to all types of relays. The S-W method is used to calculate the vectorization of the magnetic dipole after magnetization and demagnetization of nonlinear anisotropic permanent magnets. Accordingly, the virtual prototype model of the relay's static and dynamic performance characteristics is established. The electromagnetic suction force, mechanical reaction force, operating voltage, breaking speed are calculated for different voltages and rotation angles. Compared with the measured results, the maximum error is 5.01 %.
(2) The calculation accuracy of the existing agent model is poor when the performance characteristics are high dimensional, strongly nonlinear, and output zero crossing. Based on a small number of virtual prototype model calculation values, the basis function of the proxy model is obtained using fuzzy chaos expansion to correct the error between measured and the calculated results. Then, the proxy model is established. The maximum error is 6.72 %, the computational accuracy is similar to that of the virtual prototype, and the computational resource and time consumptions are less than one percent of the virtual prototype model.
(3) Based on the agent model, the formation mechanism and improvement direction of relay performance characteristics are determined from the perspectives of suction-reverse force coordination and partition kinetic energy. Meanwhile, the multi-objective differential evolution algorithm is improved to meet the demand for multi-objective optimization. The adaptive population evolution strategy and the optimal solution set screening strategy based on the idea of small habitat are proposed, which can obtain the optimal Pareto frontier solution set combination more uniformly and quickly.
(4) The iterative optimization search process avoids maturing prematurely and falling into local optimal solution sets. The extensiveness and uniformity of solution distribution are enhanced. Thus, the iterative optimization of the MLAER multi-correlation performance parameters can be ensured with accuracy and efficiency.
(5) The potential zeroing faults, such as armature neutralization and operation voltage overrun, were optimized, and the optimal mean and tolerance combinations of design parameters were given. The performance and quality consistency of the relay were improved by 16.8 % and 40 % compared with the pre-optimization period. The optimization results demonstrate the virtual prototype model considering the nonlinear permanent magnet charging and demagnetizing effects, the agent model introducing the measured results, and the differential evolution algorithm with the adaptive population strategy are effective in solving the MLAER problem.
Key wordsMagnetic latching aerospace electromagnetic relay (MLAER)    virtual prototype    surrogate model    multi-objective design optimization   
收稿日期: 2021-08-05     
PACS: TM581.3  
基金资助:国家自然科学基金资助项目(51177056)
通讯作者: 叶雪荣 男,1981年生,教授,博士生导师,研究方向为电器与电子系统全寿命周期可靠性设计理论与技术。E-mail: xuelai1981@163.com   
作者简介: 陈昊 男,1989年生,博士研究生,研究方向为航天电磁继电器可靠性评估与寿命周期质量一致性设计技术。E-mail: hao@hit.edu.cn
引用本文:   
陈昊, 叶雪荣, 梁慧敏, 翟国富. 磁保持型航天电磁继电器性能提升与质量一致性设计[J]. 电工技术学报, 2023, 38(4): 1076-1087. Chen Hao, Ye Xuerong, Liang Huimin, Zhai Guofu. Performance Enhanced and Quality Consistency Design Optimization of Magnetically Latching Aerospace Electromagnetic Relay. Transactions of China Electrotechnical Society, 2023, 38(4): 1076-1087.
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https://dgjsxb.ces-transaction.com/CN/10.19595/j.cnki.1000-6753.tces.211217          https://dgjsxb.ces-transaction.com/CN/Y2023/V38/I4/1076