旋转惯导的发展及应用
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摘要
惯性导航系统是现代各类载体的核心设备,其精度的高低制约着整个载体精度和性能的提升。旋转调制是提高惯导系统精度的一种重要误差补偿技术。本文对国内外旋转惯导的发展与应用情况进行了综述。相较于国外旋转惯导的大量成功应用,国内还需进一步提高旋转惯导的应用研究水平,以满足高精度的航海、航空以至航天领域长时间自主导航的需求。
Inertial navigation system( INS) is the core equipment of various carriers. Its precision limits the accuracy and performance of the whole carriers. Rotation modulation is one of the error compensation techniques to achieve high precision. The development and the application of rotating inertial navigation system( RINS) is reviewed at home and abroad in this paper. Compared with the successful application of RINS abroad,how to use this technology is required to further study for meeting the high precision demand of long time auto-navigation in marine,aviation and aerospace.
Inertial navigation system( INS) is the core equipment of various carriers. Its precision limits the accuracy and performance of the whole carriers. Rotation modulation is one of the error compensation techniques to achieve high precision. The development and the application of rotating inertial navigation system( RINS) is reviewed at home and abroad in this paper. Compared with the successful application of RINS abroad,how to use this technology is required to further study for meeting the high precision demand of long time auto-navigation in marine,aviation and aerospace.
引文
[1]姜复兴,庞志成.惯导测试设备原理与设计[M].哈尔滨工业大学出版社,1998:97-102.
[2]袁保伦,饶谷音.光学陀螺旋转惯导系统原理探讨[J].国防科技大学学报,2006,28(6):76-80.(Yuan Baolun,Rao Guyin. On the Theory of Optical Gyro Rotating Inertial Navigation System[J]. Journal of National University of Defense Technology,2006,28(6):76-80.)
[3] Hugh Rice,Louis Mendelsohn,Robert Aarons,Daniel Mazzola. Next Generation Marine Preeision Navigation System[J]. IEEE Position Location and Navigation Symposium. New York,2000:200-206.
[4] C. M.谢列托维奇等:陀螺系统仪表误差的自动补偿[M].国防工业出版社,1986.(C. M. Semyon Leto Vecchi. The Automatic Compensation of Gyroscope lnstrument Errors[M]. National Defense lndustry Press,1986.)
[5]高启孝.陀螺转子正、反转监控效果的研究[J].海军工程学院学报,1997,79(2):65-69.(Gao Qixiao.Research on Gyro Monitor by Changing Derection of Spin[J]. Journal of Naval Academy Of Engineering,1997,79(2):65-69.)
[6]陶冶,关劲,袁书明.惯导系统误差自补偿技术发展综述[J].导航定位与授时,2014(1):8-12.(Tao Ye,Guan Jin,Yuan Shuming. Overview for Development of Inertial Navigation System Error Self-compensation Technology[J]. Navigation Positioning&Timing,2014(1):8-12.)
[7]吴奇.旋转调制技术在MEMS捷联惯导系统中的应用与改进[D].南京,南京航空航天大学,2016.
[8]杨喆.旋转式捷联惯导系统误差分析与转动方案研究[D].哈尔滨,哈尔滨工程大学,2010.
[9]聂梦馨.单轴旋转光纤捷联惯导系统的误差建模与补偿[D].南京,南京航空航天大学,2015.
[10]陀螺仪与惯性导航专业情报网.国外惯性技术手册[M].国防工业出版社,1983:197~206.
[11]查月.舰艇惯性导航技术应用与展望[J].现代导航,2017,(2):147-151.(Zha yue. Application and Prospect of Marine Inertial Navigation Technology[J].Modern Navigation,2017,(2):147-151.)
[12]岳栋栋.光纤陀螺惯导系统对单轴旋转调制技术的适应性研究[D].中国航天科技集团公司第一研究院,2016.
[13] Terry T,Emanuel L. The AN/WSN-7B Marine Gyrocompass/navigator[C]//Proceedings of 2000 National Technical Meeting of the Institute of Navigation,2000:348-357.
[14]蔡山波.双轴旋转捷联惯导系统旋转控制算法研究[D].北京,北京理工大学,2016.
[15] Lahham J I,Brazell J R. Acoustic Noise Reduction in the MK49 Ships Inertial Navigation System[C]∥IEEE Position Location and Navigation Symposium,1992:32-39.
[16] Hibbard R,Wylie B,Levison E. Sperry Marine MK-49,the World’s Best Ring Laser Gyro Ship’s Inertial Navigation System[C]. JSDE Proceedings. Orlando,1996:132-145.
[17] Levinson Dr E,ter Horst J,Willcocks M. The Next Generation Marine Inertial Navigator is Here Now[J].IEEE Position Location and Navigation Symposium,1994:121-127.
[18]赵涛.双轴旋转光纤捷联惯导系统在线标定技术研究[D].哈尔滨,哈尔滨工程大学,2017.
[19]张凌海.激光陀螺惯性导航系统—90年代舰船导航的支柱设备[J].现代舰船,1996,(4):31-32.(Zhang Linghai. Laser Gyro Inertial Navigation SystemChief Equipment for Ship Navigation in the 1990s[J].Modern Ships,1996,(4):31-32.)
[20] Morrow R B,Heckman D W. High Precision IFOG Insertion Into the Strategic Submarine Navigation System[C]//IEEE,1998 Position Location and Navigation Symposium,1998:332-338.
[21] Heckman D W,Baretela L M. Interferometric Fiber-optic Gyro Technology[J]. IEEE Aerospace and Electronic Systems Magazine,2000,15(2):23-28.
[22]孙伟,孙枫,刘繁明.光纤陀螺旋转捷联惯导系统的发展与应用[J].传感器与微系统,2012,31(11):1-3.(Sun Wei,Sun Feng,Liu Fanming. Development and Application of FOG Rotary SINS[J]. Transducer and Microsystem Technologies,2012,31(11):1-3.)
[23] Products of Fiber-optic Inertial Navigation System“OMEGA”in the State Research Center of the Russian Federation Concern CSRI Elektropribor, JSC. 30, Malaya Posadskaya Str.,Saint Petersburg,Russian[Online],available:http://www. elektropribor. spb. ru/prod/rmiins vog 3,June 21,2012.
[24]刘灿.二频机抖激光陀螺船用捷联惯导系统的阻尼技术研究[D].长沙,国防科技大学,2013.
[25]于旭东.二频机抖激光陀螺单轴旋转惯性导航系统若干关键技术研究[D].长沙,国防科学技术大学,2011.
[26]魏国.二频机抖激光陀螺双轴旋转惯导系统若干关键技术研究[D].长沙,国防科学技术大学,2013.
[2]袁保伦,饶谷音.光学陀螺旋转惯导系统原理探讨[J].国防科技大学学报,2006,28(6):76-80.(Yuan Baolun,Rao Guyin. On the Theory of Optical Gyro Rotating Inertial Navigation System[J]. Journal of National University of Defense Technology,2006,28(6):76-80.)
[3] Hugh Rice,Louis Mendelsohn,Robert Aarons,Daniel Mazzola. Next Generation Marine Preeision Navigation System[J]. IEEE Position Location and Navigation Symposium. New York,2000:200-206.
[4] C. M.谢列托维奇等:陀螺系统仪表误差的自动补偿[M].国防工业出版社,1986.(C. M. Semyon Leto Vecchi. The Automatic Compensation of Gyroscope lnstrument Errors[M]. National Defense lndustry Press,1986.)
[5]高启孝.陀螺转子正、反转监控效果的研究[J].海军工程学院学报,1997,79(2):65-69.(Gao Qixiao.Research on Gyro Monitor by Changing Derection of Spin[J]. Journal of Naval Academy Of Engineering,1997,79(2):65-69.)
[6]陶冶,关劲,袁书明.惯导系统误差自补偿技术发展综述[J].导航定位与授时,2014(1):8-12.(Tao Ye,Guan Jin,Yuan Shuming. Overview for Development of Inertial Navigation System Error Self-compensation Technology[J]. Navigation Positioning&Timing,2014(1):8-12.)
[7]吴奇.旋转调制技术在MEMS捷联惯导系统中的应用与改进[D].南京,南京航空航天大学,2016.
[8]杨喆.旋转式捷联惯导系统误差分析与转动方案研究[D].哈尔滨,哈尔滨工程大学,2010.
[9]聂梦馨.单轴旋转光纤捷联惯导系统的误差建模与补偿[D].南京,南京航空航天大学,2015.
[10]陀螺仪与惯性导航专业情报网.国外惯性技术手册[M].国防工业出版社,1983:197~206.
[11]查月.舰艇惯性导航技术应用与展望[J].现代导航,2017,(2):147-151.(Zha yue. Application and Prospect of Marine Inertial Navigation Technology[J].Modern Navigation,2017,(2):147-151.)
[12]岳栋栋.光纤陀螺惯导系统对单轴旋转调制技术的适应性研究[D].中国航天科技集团公司第一研究院,2016.
[13] Terry T,Emanuel L. The AN/WSN-7B Marine Gyrocompass/navigator[C]//Proceedings of 2000 National Technical Meeting of the Institute of Navigation,2000:348-357.
[14]蔡山波.双轴旋转捷联惯导系统旋转控制算法研究[D].北京,北京理工大学,2016.
[15] Lahham J I,Brazell J R. Acoustic Noise Reduction in the MK49 Ships Inertial Navigation System[C]∥IEEE Position Location and Navigation Symposium,1992:32-39.
[16] Hibbard R,Wylie B,Levison E. Sperry Marine MK-49,the World’s Best Ring Laser Gyro Ship’s Inertial Navigation System[C]. JSDE Proceedings. Orlando,1996:132-145.
[17] Levinson Dr E,ter Horst J,Willcocks M. The Next Generation Marine Inertial Navigator is Here Now[J].IEEE Position Location and Navigation Symposium,1994:121-127.
[18]赵涛.双轴旋转光纤捷联惯导系统在线标定技术研究[D].哈尔滨,哈尔滨工程大学,2017.
[19]张凌海.激光陀螺惯性导航系统—90年代舰船导航的支柱设备[J].现代舰船,1996,(4):31-32.(Zhang Linghai. Laser Gyro Inertial Navigation SystemChief Equipment for Ship Navigation in the 1990s[J].Modern Ships,1996,(4):31-32.)
[20] Morrow R B,Heckman D W. High Precision IFOG Insertion Into the Strategic Submarine Navigation System[C]//IEEE,1998 Position Location and Navigation Symposium,1998:332-338.
[21] Heckman D W,Baretela L M. Interferometric Fiber-optic Gyro Technology[J]. IEEE Aerospace and Electronic Systems Magazine,2000,15(2):23-28.
[22]孙伟,孙枫,刘繁明.光纤陀螺旋转捷联惯导系统的发展与应用[J].传感器与微系统,2012,31(11):1-3.(Sun Wei,Sun Feng,Liu Fanming. Development and Application of FOG Rotary SINS[J]. Transducer and Microsystem Technologies,2012,31(11):1-3.)
[23] Products of Fiber-optic Inertial Navigation System“OMEGA”in the State Research Center of the Russian Federation Concern CSRI Elektropribor, JSC. 30, Malaya Posadskaya Str.,Saint Petersburg,Russian[Online],available:http://www. elektropribor. spb. ru/prod/rmiins vog 3,June 21,2012.
[24]刘灿.二频机抖激光陀螺船用捷联惯导系统的阻尼技术研究[D].长沙,国防科技大学,2013.
[25]于旭东.二频机抖激光陀螺单轴旋转惯性导航系统若干关键技术研究[D].长沙,国防科学技术大学,2011.
[26]魏国.二频机抖激光陀螺双轴旋转惯导系统若干关键技术研究[D].长沙,国防科学技术大学,2013.