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	Review on Developments and Progress in Nickelate-Based Heterostructure Composites and Superconducting Thin Films 期刊论文 OAI收割 ADVANCED QUANTUM TECHNOLOGIES, 2022 作者: Yang, Xiaoping; Li, Miao; Ding, Zhenyu; Li, Liangyu; Ji, Ce \| 收藏 \| 浏览/下载：50/0 \| 提交时间：2022/12/23 artificial hetero-grown materials charge transfer functional materials design nickelates orbital polarization strongly correlated electronic structures superconductivity
	Optimal design of near-earth asteroid sample-return trajectories in the sun-earth-moon system 期刊论文 iSwitch采集 Acta mechanica sinica, 2016, 卷号: 32, 期号: 4, 页码: 753-770 作者: He, Shengmao; Zhu, Zhengfan; Peng, Chao; Ma, Jian; Zhu, Xiaolong 收藏 \| 浏览/下载：39/0 \| 提交时间：2019/05/09 Near-earth asteroid Sample-return trajectory Space trajectory design competition Orbital resonance Lunar gravity assist
	Parameter optimization of passive dynamic walking biped with knees (EI CONFERENCE) 会议论文 OAI收割 2012 2nd International Conference on Materials Science and Information Technology, MSIT 2012, August 24, 2012 - August 26, 2012, Xi'an, Shaan, China 作者: Zhang P. 收藏 \| 浏览/下载：26/0 \| 提交时间：2013/03/25 A method to find the optimized parameter values of passive dynamic walking biped is presented. The effects of biped physical parameters on the stability property of passive gaits are studied by simulation experiments. The chosen parameters include the mass distribution length of leg and slope angle. The stability property of passive walking limit cycles is used as criterion of optimization calculation including the orbital stability described by eigen-values of linearized Poincare map and the global property described by size of attraction region. The simulation results show how the stability of limit cycle varies when physical parameters of the passive biped change. The work is useful to explore the inherent property of passive dynamic walking and can be used as an important instruction in the mechanical design of biped robots based on principle of passive dynamic walking. (2012) Trans Tech Publications Switzerland.
	Design and calibration of the solar irradiance monitor (EI CONFERENCE) 会议论文 OAI收割 International Symposium on Photoelectronic Detection and Imaging 2011: Space Exploration Technologies and Applications, May 24, 2011 - May 26, 2011, Beijing, China 作者: Yang D.-J.; Gong C.-H.; Wang Y.-P.; Ye X.; Fang W. 收藏 \| 浏览/下载：39/0 \| 提交时间：2013/03/25 The solar irradiance monitor (SIM) with the design accuracy of 5 used to monitor the secular changes of the total solar irradiance on FY-3 satellite takes the sun-scanning measurement method on-orbit. Compared to the sun-tracking measurement method this method simplifies the structure and cuts the cost but the measuring accuracy is affected by the sun-synchronous orbit sunlight incidence angle and the installing angle of the SIM in the satellite. Through the ground calibration experiment studies on the affection of different sunlight incidence angles to the measurement accuracy. First by the satellite tool kit (STK) simulation software simulates the orbital parameters of the sun-synchronous satellite and calculates the Sun ascension and declination at any time. By the orbit coordinate transformation matrix gets the components of the Sun vectors to the axes of the satellite and base on the components designs the field of view and the installing angles of the SIM. Then designs and completes the calibration experiment to calibrate the affection of the incidence angles. Selecting 11 different angles between the sunlight and the satellite X-axis measures the total solar irradiance by the SIM at each angle and compares to the irradiances of the SIAR reference radiometers and gets the coefficient curves of the three channels of the SIM. Finally by the quadratic fitting gets the correction equations on the incidence angles: R 1=5.7110-52 -2.45310 -3+1.0302 R2=2.8410-5-1. 96510-3+1.0314 and R3 =1.7210 -52-4.18410-4+0.9946. The equations will aimprove the on-orbit measurement accuracy of the solar irradiance and are very important to the on-orbit data processing after the satellite launched. 2011 SPIE.
	Orbit design for the Laser Interferometer Space Antenna (LISA) 期刊论文 OAI收割 SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2010, 卷号: 53, 期号: 1, 页码: 179-186 作者: Xia Yan; Li GuangYu; Heinzel, Gerhard; Ruediger, Albrecht; Luo YongJie 收藏 \| 浏览/下载：46/0 \| 提交时间：2011/11/23 co-orbital restricted problem orbit design orbit optimization launch energy
	Coorbital restricted problem and its application in the design of the orbits of the LISA spacecraft 期刊论文 OAI收割 INTERNATIONAL JOURNAL OF MODERN PHYSICS D, 2008, 卷号: 17, 期号: 7, 页码: 1005-1019 作者: 收藏 \| 浏览/下载：24/0 \| 提交时间：2011/12/29 restricted problem coorbital restricted problem LISA constellation orbital design