基于液晶光阀的星模拟器研究
摘要
星模拟器是卫星控制系统中姿态测量关键部件——星敏感器的一项重要地面试验设备。星敏感器地面标定试验精度的高低,将直接影响卫星在轨道上的工作精度。本文实现在地面上模拟卫星在太空中所看到的恒星,研究了一种卫星试验用星模拟器,解决了星敏感器地面模拟试验测试的问题。
本文论述了星模拟器的组成、总体结构和星模拟器的基本功能,并对星模拟器光学系统、液晶光阀星图显示、系统精度进行了深入的研究。提出了一种基于液晶光阀的高精度星图模拟方法。液晶光阀是星模拟器中最重要的部件,通过对星光模拟和星等分等设计,利用液晶光阀实现高质量的星图动态显示。通过星间角距和星等的检测与分析验证了星模拟器的精度的准确性,为星模拟器的研究提供了设计依据。
The star simulator instrument is an important test equipment on the ground of star sensitivity instrument which is a stance test key component in planet control system. Whether star sensitivity instrument demarcate test precision high or not, will directly affect work precision work the planet on the orbit. to simulate the earth on the ground which can be seen in firmament, This paper advances a miniature collimating infrared star simulator design , solves the star sensor ground simulation test question.
This paper introduces the compose, integer structure, star simulator, and based function of the star simulator instrument and shows a detailed exposition about optical system design liquid crystal light valve display and system accuracy. This paper presents a liquid crystal light valve based on the high-precision satellite image simulation methods. LCLV is the most important components of star simulator, through sub-stars such as simulation and design, use of high-quality liquid crystal light valve dynamic display the star map; via satellite from the angle between the satellites and the detection and analysis of test the accuracy of the satellite simulator the accuracy of satellite simulator for the study of the design basis.
本文论述了星模拟器的组成、总体结构和星模拟器的基本功能,并对星模拟器光学系统、液晶光阀星图显示、系统精度进行了深入的研究。提出了一种基于液晶光阀的高精度星图模拟方法。液晶光阀是星模拟器中最重要的部件,通过对星光模拟和星等分等设计,利用液晶光阀实现高质量的星图动态显示。通过星间角距和星等的检测与分析验证了星模拟器的精度的准确性,为星模拟器的研究提供了设计依据。
The star simulator instrument is an important test equipment on the ground of star sensitivity instrument which is a stance test key component in planet control system. Whether star sensitivity instrument demarcate test precision high or not, will directly affect work precision work the planet on the orbit. to simulate the earth on the ground which can be seen in firmament, This paper advances a miniature collimating infrared star simulator design , solves the star sensor ground simulation test question.
This paper introduces the compose, integer structure, star simulator, and based function of the star simulator instrument and shows a detailed exposition about optical system design liquid crystal light valve display and system accuracy. This paper presents a liquid crystal light valve based on the high-precision satellite image simulation methods. LCLV is the most important components of star simulator, through sub-stars such as simulation and design, use of high-quality liquid crystal light valve dynamic display the star map; via satellite from the angle between the satellites and the detection and analysis of test the accuracy of the satellite simulator the accuracy of satellite simulator for the study of the design basis.
引文
[1].张文明,林玲,郝永杰等.小型星模拟器中星图动态显示系统的设计.光电工程,2000,No.5:11-14
[2].宋晓龙.全轨道实时星模拟器.系统仿真学报,1995.No.6:40-46
[3].潘平.单星模拟数字光源研制技术:[硕士学位毕业论文].西安:中国科学院西安光学精密机械研究所,2005
[4].王兆魁,张育林.面向空间目标监视的星图模拟器设计与实现.系统仿真学报,2006,NO.5:1195-1211
[5].钟奉金,许世文,赵亮等.星模拟器中积分球内光纤端面有效照度的计算.哈尔滨工业大学学报,1998,No.4:112-115
[6].田金文,欧阳桦,郑胜等.一种星图中星的提取方法.华中科技大学学报,2005,No.4:38-40
[7].王南华,张陶,赵旭行小型动态模拟器设计.航天设计,1996.No.4:13-21
[8].田玉龙.王广君,房建成等.星光模拟的半物理仿真技术.中国航天,2004,No.4:25-26
[9].许世文,龙夫年,付苓等.实时星场模拟器中的坐标变换.哈尔滨工业大学学报,1998,No.5:118-121
[10].朱长征.基于星模拟器的星模式算法及空间飞行器姿态确定技术研究:[博士学位毕业论文].合肥:国防科技大学,2004
[11].张文明小型星模拟器的研制方法和研制技术[工程硕士学位论文].电子科技大学.2003
[12].全伟,房建成.高精度星图模拟及有效性验证新方法.光电工程,2005.No.7:22-2
[13].朱膏祥.白天用CCD摄像机对天体目标的探测及实验.光电工程,1995,Vol.22,No.6:1-10.
[14].杨威,赵健翔.面阵CCD电子线路在星敏感器设计中的应用.控制工程,1996,No.3:24-29
[15].伊世同.全天星图.北京:科学出版社,1983:1-50
[16].Kurii,Toshihiro.Next generation at Titude control with scan-through earth sensor and disturbance suppression.In:AIAA,International Communications Satellite Systems Conference and Exhibit,17th,Yokohama,Japan,Feb.23-27,1998,661-669
[17].James J.Lisowski,SciTec;Michelle A.Najarian,SciTec.Spectrometer channel characterization for the Airborne Remote earth sensor(ARES).Hyperspectral Remote Sensing and Applications Meeting1996,2821(1):204-214
[18].孙萍.液晶光阀实时图像变换实验的新内容.物理实验,2005,NO.5:4-7.
[19].孙雷,陈少文,马秀芳.读出光光源对液晶光阀实验的影响.物理实验,2005,No.10:45-48.
[20].朱长征,沈振康.面向星敏感器的星模式识别算法冲国惯性技术学报,2004,No.2.55-61
[21].黄种,周学平,欧阳艳东等.液晶光阀的电光色散特性研究.光谱学与光谱分析,2006,No.3:539-542.
[22].张磊,,祁康成,成建波.液晶光阀复合光吸收层的吸收系数研究.光电子技术,2005,No.4:222-225.
[23].钱祥忠,黄芳云.液晶光阀光电导层光吸收系数的研究.液晶与显示,2004,No.4:218-221.
[24].张钧萍.一种模拟CCD星图的方法.中国空间科学技术,1999,No.3;46-50.
[25].林涛.四边形全天自主星图识别算法.宇航学报,2000,No.2:82-85.
[26].卢欣.CCD星敏感器光学系统设计.中国空间技术,1994,No.8:49-55
[27].钱祥忠.液晶光阀中的高反射介质镜的研究.液晶显示与器件,2002,No.2:43-48.
[28].王红霞,何俊发,李俊等.基于液晶光阀微分处理的实时联合变换相关器.光电工程,2004,No.10:57-60.
[29].于永红,杜丕一,王瑞春等.复合光导层液晶光阀的研究功能材料与器件学报,2003,No.3:305-308
[30].郝雪涛,张广军,江洁.星敏感器模型参数分析与校准方法研究,2005,No.3:5-10
[31].沈大可,韩高荣,杜丕一.液晶光阀薄膜的光电特性研究.功能材料与器件学报,2002,No.4:335-400。
[32].祁康成,光寻址液晶光阀的吸收层.真空科学与技术,2002,NO,12:60-63.
[33].T.K Alex;J.A.Kamalakar.Scanning infrared earth sensor for INSAT-Ⅱ.sensors and sensor Systems for Guidance and Navigation Meeting 1991,106-111
[34].Rdbert R.Strunce,Jr,Francis H,Maher,An Object Oriented Dynatnic Simulation Architecture For Rapid Spacecraft Prototyping,PWSPublishing Co.1997.
[35].Robbie E.Hood and Roy W.Spencer,High Altitude Aircraft Mapping of Near Surface Ocean Winds,0-7803-3068-4/9655.000 1996 IEEE
[36].Uwe Schmidt,Intelligent error correction method applied on active pixel sensor based star tracker,Detectors and Associated Signal Processing Ⅱ,edited by Jean-Pierre Chatard,Peter N.J.Dennis,Proc.of SPIE Vol.5964,59640J,
[37].Ahmed Salah;Ashraf Adel;Ahmed Ezeidin.Design and Implementation of an Area-Efficient MEMS-Based IR Static earthsensor.The 15th International Conference on Microelectronics 2003,143-146
[38].Kenichiro Nigo;Ritsno Hasegawa;Toshihiro Kurii;Masanori Fukui.Reduction of earth sensor Random Error Caused by Minute Vibration Interference.AIAA Guidance,Navigation and Control Confereoce2002,2468-2475
[39].G Soto-Romero;F.Bony;JJ.Simonne;JY.Fonrniol.Micro Infrared earth sensor project:an integrated IR camera for earth remotesensing,sensors,systems,and next-generation satellites V2001,176-187
[40].K.Kanakaraj;J,A.Kamalakar;A.S.Laxmiprasad.Infrared earth sensor for detection of solar sail deployment of INSAT-2A.Space Guidance,Control,and Tracking Meeting 1993,1949(1):266-271
[41].Todd J.Bednarek.Dual cone scanning earth sensor processing algorithms.Small Satellite Technologies and Applications Ⅱ Meeting1 992,1691(1):181-191
[42].George Rullman;Richard Burton;Len Anderson.A novel new geo earth sensor provides high accuracy.Proceedings of the Annual American Astronautically Society Rocky Mountain Guidance and Control Conference held February 2-6,2000,447-464
[2].宋晓龙.全轨道实时星模拟器.系统仿真学报,1995.No.6:40-46
[3].潘平.单星模拟数字光源研制技术:[硕士学位毕业论文].西安:中国科学院西安光学精密机械研究所,2005
[4].王兆魁,张育林.面向空间目标监视的星图模拟器设计与实现.系统仿真学报,2006,NO.5:1195-1211
[5].钟奉金,许世文,赵亮等.星模拟器中积分球内光纤端面有效照度的计算.哈尔滨工业大学学报,1998,No.4:112-115
[6].田金文,欧阳桦,郑胜等.一种星图中星的提取方法.华中科技大学学报,2005,No.4:38-40
[7].王南华,张陶,赵旭行小型动态模拟器设计.航天设计,1996.No.4:13-21
[8].田玉龙.王广君,房建成等.星光模拟的半物理仿真技术.中国航天,2004,No.4:25-26
[9].许世文,龙夫年,付苓等.实时星场模拟器中的坐标变换.哈尔滨工业大学学报,1998,No.5:118-121
[10].朱长征.基于星模拟器的星模式算法及空间飞行器姿态确定技术研究:[博士学位毕业论文].合肥:国防科技大学,2004
[11].张文明小型星模拟器的研制方法和研制技术[工程硕士学位论文].电子科技大学.2003
[12].全伟,房建成.高精度星图模拟及有效性验证新方法.光电工程,2005.No.7:22-2
[13].朱膏祥.白天用CCD摄像机对天体目标的探测及实验.光电工程,1995,Vol.22,No.6:1-10.
[14].杨威,赵健翔.面阵CCD电子线路在星敏感器设计中的应用.控制工程,1996,No.3:24-29
[15].伊世同.全天星图.北京:科学出版社,1983:1-50
[16].Kurii,Toshihiro.Next generation at Titude control with scan-through earth sensor and disturbance suppression.In:AIAA,International Communications Satellite Systems Conference and Exhibit,17th,Yokohama,Japan,Feb.23-27,1998,661-669
[17].James J.Lisowski,SciTec;Michelle A.Najarian,SciTec.Spectrometer channel characterization for the Airborne Remote earth sensor(ARES).Hyperspectral Remote Sensing and Applications Meeting1996,2821(1):204-214
[18].孙萍.液晶光阀实时图像变换实验的新内容.物理实验,2005,NO.5:4-7.
[19].孙雷,陈少文,马秀芳.读出光光源对液晶光阀实验的影响.物理实验,2005,No.10:45-48.
[20].朱长征,沈振康.面向星敏感器的星模式识别算法冲国惯性技术学报,2004,No.2.55-61
[21].黄种,周学平,欧阳艳东等.液晶光阀的电光色散特性研究.光谱学与光谱分析,2006,No.3:539-542.
[22].张磊,,祁康成,成建波.液晶光阀复合光吸收层的吸收系数研究.光电子技术,2005,No.4:222-225.
[23].钱祥忠,黄芳云.液晶光阀光电导层光吸收系数的研究.液晶与显示,2004,No.4:218-221.
[24].张钧萍.一种模拟CCD星图的方法.中国空间科学技术,1999,No.3;46-50.
[25].林涛.四边形全天自主星图识别算法.宇航学报,2000,No.2:82-85.
[26].卢欣.CCD星敏感器光学系统设计.中国空间技术,1994,No.8:49-55
[27].钱祥忠.液晶光阀中的高反射介质镜的研究.液晶显示与器件,2002,No.2:43-48.
[28].王红霞,何俊发,李俊等.基于液晶光阀微分处理的实时联合变换相关器.光电工程,2004,No.10:57-60.
[29].于永红,杜丕一,王瑞春等.复合光导层液晶光阀的研究功能材料与器件学报,2003,No.3:305-308
[30].郝雪涛,张广军,江洁.星敏感器模型参数分析与校准方法研究,2005,No.3:5-10
[31].沈大可,韩高荣,杜丕一.液晶光阀薄膜的光电特性研究.功能材料与器件学报,2002,No.4:335-400。
[32].祁康成,光寻址液晶光阀的吸收层.真空科学与技术,2002,NO,12:60-63.
[33].T.K Alex;J.A.Kamalakar.Scanning infrared earth sensor for INSAT-Ⅱ.sensors and sensor Systems for Guidance and Navigation Meeting 1991,106-111
[34].Rdbert R.Strunce,Jr,Francis H,Maher,An Object Oriented Dynatnic Simulation Architecture For Rapid Spacecraft Prototyping,PWSPublishing Co.1997.
[35].Robbie E.Hood and Roy W.Spencer,High Altitude Aircraft Mapping of Near Surface Ocean Winds,0-7803-3068-4/9655.000 1996 IEEE
[36].Uwe Schmidt,Intelligent error correction method applied on active pixel sensor based star tracker,Detectors and Associated Signal Processing Ⅱ,edited by Jean-Pierre Chatard,Peter N.J.Dennis,Proc.of SPIE Vol.5964,59640J,
[37].Ahmed Salah;Ashraf Adel;Ahmed Ezeidin.Design and Implementation of an Area-Efficient MEMS-Based IR Static earthsensor.The 15th International Conference on Microelectronics 2003,143-146
[38].Kenichiro Nigo;Ritsno Hasegawa;Toshihiro Kurii;Masanori Fukui.Reduction of earth sensor Random Error Caused by Minute Vibration Interference.AIAA Guidance,Navigation and Control Confereoce2002,2468-2475
[39].G Soto-Romero;F.Bony;JJ.Simonne;JY.Fonrniol.Micro Infrared earth sensor project:an integrated IR camera for earth remotesensing,sensors,systems,and next-generation satellites V2001,176-187
[40].K.Kanakaraj;J,A.Kamalakar;A.S.Laxmiprasad.Infrared earth sensor for detection of solar sail deployment of INSAT-2A.Space Guidance,Control,and Tracking Meeting 1993,1949(1):266-271
[41].Todd J.Bednarek.Dual cone scanning earth sensor processing algorithms.Small Satellite Technologies and Applications Ⅱ Meeting1 992,1691(1):181-191
[42].George Rullman;Richard Burton;Len Anderson.A novel new geo earth sensor provides high accuracy.Proceedings of the Annual American Astronautically Society Rocky Mountain Guidance and Control Conference held February 2-6,2000,447-464