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飞渡,撷取彼岸花
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作者 雨潇 《初中数学辅导(初中版)》 2011年第6期1-1,共1页
先秦《苻子》一书中有一个“后羿射箭”的故事。夏朝的后羿是一位神射手,他练就了一身百步穿杨的好本领,立射、跪射、骑射样样精通,而且箭箭都射中靶心,几乎从来没有失过手。一日,夏王让后羿表演箭术,夏王对他说:
关键词 中学 课外阅读 阅读材料 《飞渡 撷取彼岸花》
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Welding characteristics of AZ31B magnesium alloy using DC-PMIG welding 被引量:4
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作者 张兆栋 刘黎明 宋刚 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2013年第2期315-322,共8页
Direct current pulsed metal inert-gas (DC-PMIG) welding was carried out on AZ31B magnesium alloy to obtain continuous welding joints of 3 mm and 8 mm thickness with 1.6 mm diameter of filler wire. The behavior and m... Direct current pulsed metal inert-gas (DC-PMIG) welding was carried out on AZ31B magnesium alloy to obtain continuous welding joints of 3 mm and 8 mm thickness with 1.6 mm diameter of filler wire. The behavior and mechanism of metal transfer, the parameter ranges of stable welding process, the microstructure and mechanical properties of magnesium alloy were investigated. The results show that the metal transfer form of magnesium alloy using DC-PMIG welding is realized in modes of globular transfer, projected transfer and spray transfer. Welding spatter with a large size will be produced in the mode of globular transfer, and high-quality joints with few spatters can be obtained in the mode of projected transfer and spray transfer when the linear energy of filler wire is 242-27l J/cm, droplet diameter is 1.6-0.9 mm tensile strength of weld beads is 94.2% of that of base metals. and transition frequency is 30-69 Hz. The average ultimate 展开更多
关键词 AZ31B magnesium alloy DC-PMIG welding metal transfer welding spatter
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Transition Stage Control of Tail Sitter Aircraft Based on Guardian Maps
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作者 ZHANG Yong CHEN Xinyi 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2020年第2期322-331,共10页
To deal with the high nonlinearities and strong couplings in the transition stage of tailsitter aircraft,an adaptive gainscheduling controller is proposed by combining the guardian maps theory and H∞control theory.Th... To deal with the high nonlinearities and strong couplings in the transition stage of tailsitter aircraft,an adaptive gainscheduling controller is proposed by combining the guardian maps theory and H∞control theory.This method is applied to track the flightpath angle of the transition stage of tailsitter aircraft,and compared with the linear quadratic regulator(LQR)method based on traditional gain scheduling.Simulation results show that the controller based on the guardian maps theory can autonomously schedule the appropriate control parameters and accomplish the stable transition.Besides,the proposed method shows better tracking performance than the LQR method based on traditional gain scheduling. 展开更多
关键词 tailsitter aircraft transition stage guardian maps adaptive gainscheduling controller
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