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浏览/检索结果: 共4条，第1-4条 帮助 限定条件 内容类型：会议论文    专题：长春光学精密机械与物理研究所    第一署名单位    第一作者单位    通讯作者单位     已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Design and calibration of the solar irradiance monitor (EI CONFERENCE) 会议论文 International Symposium on Photoelectronic Detection and Imaging 2011: Space Exploration Technologies and Applications, May 24, 2011 - May 26, 2011, Beijing, China Yang D.-J.; Fang W.; Ye X.; Wang Y.-P.; Gong C.-H.; Zhang G.-W. 收藏  |  浏览/下载：16/0  |  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.   The masks fabricated by UV LIGA for excimer laser ablation and X-ray lithography 会议论文 2004 Liang J. Q.; Le Z. C.; Wang W. B.; Peng L. Q.; Lan W. H.; Ming A. J.; Ye J.; Quan B. S.; Yao J. S.; Xuan M.; Wang L. J. 收藏  |  浏览/下载：9/0  |  提交时间：2013/03/28 The study on the compound X-ray refractive lens using LIGA technique 会议论文 2004 Liang J. Q.; Le Z. C.; Peng L. Q.; Wang W. B.; Lan W. H.; Ming A. J.; Yi F. T.; Ye J.; Quan B. S.; Yao J. S.; Xuan M.; Wang L. J. 收藏  |  浏览/下载：12/0  |  提交时间：2013/03/28 Dispersion and nonlinear decaying properties of corona-poled NPP side-chain polymer waveguides 会议论文 1996 Gao F. B.; Jin F.; Xing R. B.; Lin J. L.; Ye C.; Feng X. M. 收藏  |  浏览/下载：11/0  |  提交时间：2013/03/28