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Electrically controllable spin filtering in zigzag phosphorene nanoribbon based normal–antiferromagnet–normal junctions
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作者 李锐岗 刘军丰 汪军 《Chinese Physics B》 SCIE EI CAS CSCD 2024年第1期666-670,共5页
We investigated the electric controllable spin-filtering effect in a zigzag phosphorene nanoribbon(ZPNR) based normal–antiferromagnet–normal junction. Two ferromagnets are closely coupled to the edges of the nanorib... We investigated the electric controllable spin-filtering effect in a zigzag phosphorene nanoribbon(ZPNR) based normal–antiferromagnet–normal junction. Two ferromagnets are closely coupled to the edges of the nanoribbon and form the edge-to-edge antiferromagnetism. Under an in-plane electric field, the two degenerate edge bands of the edge-to-edge antiferromagnet split into four spin-polarized sub-bands and a 100% spin-polarized current can be easily induced with the maximal conductance 2e~2/h. The spin polarization changes with the strength of the electric field and the exchange field,and changes sign at opposite electric fields. The spin-polarized current switches from one edge to the other by reversing the direction of the electric field. The edge current can also be controlled spatially by changing the electric potential of the scattering region. The manipulation of edge current is useful in spin-transfer-torque magnetic random-access memory and provides a practical way to develop controllable spintronic devices. 展开更多
关键词 zigzag phosphorene electrically controllable spin filter quantum transport
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Second order sliding mode control with back stepping approach for moving mass spinning missiles
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作者 郭鹏飞 杨树兴 赵良玉 《Journal of Beijing Institute of Technology》 EI CAS 2016年第1期17-22,共6页
An attitude controller using the second order sliding mode control methodology with a backstepping approach(SOSMCB)is designed and implemented for a spinning missile with two internal moving mass blocks.The system c... An attitude controller using the second order sliding mode control methodology with a backstepping approach(SOSMCB)is designed and implemented for a spinning missile with two internal moving mass blocks.The system consists of a rigid body and two radial internal moving mass blocks and its mathematical model is established based on Newtonian mechanics.The control scheme integrates a second order sliding mode control algorithm into the last step of the backstepping approach,and its stability is proved by means of a Lyapunov function.The performance of the controller is demonstrated by numerical simulations,the results show that the attitude controller is stable and effective. 展开更多
关键词 spinning missile moving mass backstepping second order sliding mode control
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Controlling spins in silicon quantum dots
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作者 Haiou Li Xin Zhang Guoping Guo 《Journal of Semiconductors》 EI CAS CSCD 2020年第7期4-6,共3页
Spins in silicon(Si)quantum dots(QDs),as a new type of solid state qubits,is expected to be a competitive contender in the long run of scalable quantum computation[1].Quantum computation is believed to be the next-gen... Spins in silicon(Si)quantum dots(QDs),as a new type of solid state qubits,is expected to be a competitive contender in the long run of scalable quantum computation[1].Quantum computation is believed to be the next-generation computing technology to solve the problems that no classical computer can feasibly tackle.In the last decade. 展开更多
关键词 controlling spins SILICON quantum dots
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Nutation instability of spinning solid rocket motor spacecraft 被引量:1
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作者 Dan YANG Yongliang XIONG +1 位作者 Qian REN Xianyong WANG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2017年第4期1363-1372,共10页
The variation of mass, and moment of inertia of a spin-stabilized spacecraft leads to concern about the nutation instability. Here a careful analysis on the nutation instability is performed on a spacecraft propelled ... The variation of mass, and moment of inertia of a spin-stabilized spacecraft leads to concern about the nutation instability. Here a careful analysis on the nutation instability is performed on a spacecraft propelled by solid rocket booster(SRB). The influences of specific solid propellant designs on transversal angular velocity are discussed. The results show that the typical SRB of End Burn suppresses the non-principal axial angular velocity. On the contrary, the frequently used SRB of Radial Burn could amplify the transversal angular velocity. The nutation instability caused by a design of Radial Burn could be remedied by the addition of End Burn at the same time based on the study of the combination design of both End Burn and Radial Burn.The analysis of the results proposes the design conception of how to control the nutation motion.The method is suitable to resolve the nutation instability of solid rocket motor with complex propellant patterns. 展开更多
关键词 Attitude control Nutation dampers Payloads Solid rocket booster Spin stabilization of spacecraft
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Valley photonic crystals for control of spin and topology
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《Science Foundation in China》 CAS 2017年第1期7-8,共1页
Subject Code:A04With the support by the National Natural Science Foundation of China,the research team led by Prof.Dong Jianwen(董建文)at the State Key Laboratory of Optoelectronic Materials and Technologies&Schoo... Subject Code:A04With the support by the National Natural Science Foundation of China,the research team led by Prof.Dong Jianwen(董建文)at the State Key Laboratory of Optoelectronic Materials and Technologies&School of Physics,Sun Yat-sen University,discovered the control of spin and topology in valley photonic crystals,which was published in Nature Materials(2017,DOI:10.1038/NMAT4087). 展开更多
关键词 Valley photonic crystals for control of spin and topology
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