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Mechanisms of ductile-to-brittle transition in Sn−3.0Ag−0.5Cu solder alloy at cryogenic temperature
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作者 Sheng-li LI Chun-jin HANG +7 位作者 Qi-long GUAN Xiao-jiu TANG Ning ZHOU Yan-hong TIAN Wei ZHANG Dan YU Ying DING Xiu-li WANG 《Transactions of Nonferrous Metals Society of China》 2025年第4期1281-1291,共11页
The inherent brittle behavior and ductile-to-brittle transition(DBT)mechanism of Sn−3.0Ag−0.5Cu(SAC305)solder alloy at the liquid nitrogen temperature(LNT,77 K)were investigated through uniaxial tensile experiments co... The inherent brittle behavior and ductile-to-brittle transition(DBT)mechanism of Sn−3.0Ag−0.5Cu(SAC305)solder alloy at the liquid nitrogen temperature(LNT,77 K)were investigated through uniaxial tensile experiments conducted at different temperatures.Dynamic recovery and recrystallization of SAC305 solder alloy at room temperature(RT,293 K)activate a softening process.Conversely,intersecting and none-intersecting deformation twins,embedded in body-centered tetragonal Sn,enhance tensile strength and stabilize strain hardening rate,while suppressing the elongation of the alloy at LNT.The irreconcilable velocity difference between twin thickening(~8μm/s)and dislocation slip(4μm/s)results in premature brittle fracture,during the linear hardening and DBT.Moreover,the secondary phases degrade the mechanical property of SAC305 solder alloy,and micro-cracks appear between Cu_(6)Sn_(5)and Ag_(3)Sn in the eutectic matrix. 展开更多
关键词 SAC305 deformation twinning secondary phases tensile property cryogenic temperature
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Data⁃Based Feedback Relearning Algorithm for Robust Control of SGCMG Gimbal Servo System with Multi⁃source Disturbance 被引量:3
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作者 ZHANG Yong MU Chaoxu LU Ming 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2021年第2期225-236,共12页
Single gimbal control moment gyroscope(SGCMG)with high precision and fast response is an important attitude control system for high precision docking,rapid maneuvering navigation and guidance system in the aerospace f... Single gimbal control moment gyroscope(SGCMG)with high precision and fast response is an important attitude control system for high precision docking,rapid maneuvering navigation and guidance system in the aerospace field.In this paper,considering the influence of multi-source disturbance,a data-based feedback relearning(FR)algorithm is designed for the robust control of SGCMG gimbal servo system.Based on adaptive dynamic programming and least-square principle,the FR algorithm is used to obtain the servo control strategy by collecting the online operation data of SGCMG system.This is a model-free learning strategy in which no prior knowledge of the SGCMG model is required.Then,combining the reinforcement learning mechanism,the servo control strategy is interacted with system dynamic of SGCMG.The adaptive evaluation and improvement of servo control strategy against the multi-source disturbance are realized.Meanwhile,a data redistribution method based on experience replay is designed to reduce data correlation to improve algorithm stability and data utilization efficiency.Finally,by comparing with other methods on the simulation model of SGCMG,the effectiveness of the proposed servo control strategy is verified. 展开更多
关键词 control moment gyroscope feedback relearning algorithm servo control reinforcement learning multisource disturbance adaptive dynamic programming
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基于积分终端滑模的SGCMG伺服系统抗干扰控制
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作者 鲁明 宿诺 +3 位作者 赵维珩 曹歌 田利梅 张强 《航空学报》 CSCD 北大核心 2024年第S1期335-345,共11页
单框架控制力矩陀螺(SGCMG)是空间飞行器姿态控制的重要组成部分。对柔性隔振器和太空中存在的未知干扰影响,设计了一种基于积分终端滑模控制器(ITSMC)和有限时间干扰观测器(FTDO)的复合控制方案,它能够消除柔性隔振器中存在的不确定干... 单框架控制力矩陀螺(SGCMG)是空间飞行器姿态控制的重要组成部分。对柔性隔振器和太空中存在的未知干扰影响,设计了一种基于积分终端滑模控制器(ITSMC)和有限时间干扰观测器(FTDO)的复合控制方案,它能够消除柔性隔振器中存在的不确定干扰,并在收敛时间内达到期望速度。与传统PI控制器相比,设计的积分终端滑模的波动幅度和振荡频率更低,稳态误差≤0.032,调节时间快40%,超调量降低24%,抗扰能力更强;在积分末端滑模控制器上设计有限时间观测器进行抗干扰补偿,组成的复合控制器稳态误差再次缩小不超过0.003,超调量降低至1%,具有低抖震、强抗干扰效果,对于空间中存在的未知干扰进行了有力的消除。最后,通过MATLAB仿真验证了上述方法可以达到预期效果。 展开更多
关键词 单框架控制力矩陀螺 柔性支撑动态 积分终端滑模 干扰观测器 抗干扰
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