半球谐振陀螺发展综述
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摘要
首先阐述了半球谐振陀螺工作原理及技术优势,后着重对其在美国、俄罗斯、法国的发展历程、应用场景、技术发展、精度指标及进行了综述,同时概述了国内的发展历程、现阶段达到水平。其后,针对海上领域武器系统的特点及需求,在借鉴国外已有应用的基础上,论述半球谐振陀螺在海上应用的可能性及优势。最后对半球谐振陀螺的未来发展进行了展望。
This paper first expounds the working principle and technical advantages of the hemispherical resonant gyro.After that,it focuses on its development history,application scenarios,technological development,and accuracy indicators in the United States,Russia,and France.It also outlines the domestic development process and current level.Then,in view of the characteristics and needs of weapons systems in the maritime field,on the basis of the existing applications in foreign countries,the possibility and advantages of the hemispherical resonant gyro in offshore applications are discussed.Finally,the future development of the hemispherical resonant gyro is prospected.
This paper first expounds the working principle and technical advantages of the hemispherical resonant gyro.After that,it focuses on its development history,application scenarios,technological development,and accuracy indicators in the United States,Russia,and France.It also outlines the domestic development process and current level.Then,in view of the characteristics and needs of weapons systems in the maritime field,on the basis of the existing applications in foreign countries,the possibility and advantages of the hemispherical resonant gyro in offshore applications are discussed.Finally,the future development of the hemispherical resonant gyro is prospected.
引文
[1]潘瑶,曲天良,杨开勇,等.半球谐振陀螺研究现状与发展趋势[J].导航定位与授时,2017,4(2):9-13.
[2] Matthews A,Rybak F J.Comparison of hemispherical resonator gyro and optical gyros[J].Aerospace&Electronic Systems Magazine IEEE,1992,7(5):40-46.
[3] Lynch D,Matthews A,Varty G T.Innovative mechanization to optimize inertial sensors for high or low rate operations[J].Symposium Gyro Techonology,1997,16(9):1-9.
[4] Anon.Northrop Grunnan′s hemispherical resonator GYRO matks 30 million operating hours in space[DB/OL].[2016-01-29].http://news.northropgrumman.com/news/releases/northrp-grumman-s-hemispherical-resonator-gyro-marks-30-million-operatinghours-in-space.
[5]沈博昌,伊国兴,任顺清,等.半球谐振陀螺仪谐振子振动特性的有限元分析[J].中国惯性技术学报,2004,12(6):56-60.
[6]周小刚,汪立新,方针,等.半球谐振陀螺平台调平系统设计及仿真[J].宇航学报,2011,32(3):549-553.
[7]高胜利.半球谐振陀螺的分析与设计[D].哈尔滨:哈尔滨工程大学,2008.
[8]杨倩.基于半球谐振陀螺的惯性导航系统研究[D].哈尔滨:哈尔滨工业大学,2009:16-22.
[9]祁家毅,任顺清,冯士伟,等.半球谐振陀螺仪随机误差分析[J].中国惯性技术学报,2009,17(1):98-101.
[10]高胜利,吴简彤.基于多电极的半球谐振陀螺信号检测[J].哈尔滨工程大学学报,2008,29(5):474-478.
[11]雷霆.半球谐振陀螺控制技术研究[D].重庆:重庆大学,2006.
[12]赵洪波.半球谐振陀螺仪误差机理分析与误差抑制方法研究[D].哈尔滨:哈尔滨工业大学,2013.
[13]倪受东,吴洪涛,嵇海平,等.微型半球陀螺仪的误差源研究[J].传感器与微系统,2007,26(1):30-32.
[14] Remillieux G,Goudon J C,Roberfroid D.Coriolisvibrating gyros for aeronautical applications[R].SAE Technical Paper,2011.
[15] Jeanroy A,Bouvet A,Remillieux G.HRG and marine applications[J].Gyroscopy and Navigation,2014,5(2):67-74.
[16] Rozelle D M.The hemispherical resonator gyro:From wineglass to the planets[C]//Proceedings of19th AAS/AIAA Space Flight Mechanics Meeting.2009:1157-1178.
[17] Remillieux G,Delhaye F.Sagem Coriolis Vibrating Gyros:a vision realized[C]//2014 DGON Inertial Sensors and Systems Symposium(ISS).IEEE,2014:1-13.
[18] Remillieux G,Delhaye F.Sagem Coriolis Vibrating Gyros:a vision realized[C]//2014 DGON Inertial Sensors and Systems Symposium(ISS).IEEE,2014:1-13.
[19] Lenoble A,Rouilleault T.PRIMUS:SWAP-oriented IMUs for multiple applications[C]//2016DGON Intertial Sensors and Systems(ISS).IEEE,2016:1-16.
[20] http://www.northropgrumman.com/Capabilities/SIRU/Documents/Scalable_SIRU_Family.pdf.
[21] Trusov A A,Meyer A D,Mccammon G H,et al.Toward software defined coriolis vibratory gyroscopes with dynamic self-calibration[C]//2016DGON Intertial Sensors and Systems(ISS).IEEE,2016:1-11.
[22] Remillieux G,Delhaye F.Sagem Coriolis Vibrating Gyros:a vision realized[C]//2014 DGON Inertial Sensors and Systems Symposium(ISS).IEEE,2014:1-13.
[23] Jeanroy A,Grosset G,Goudon J C,et al.HRG by Sagem from laboratory to mass production[C]//2016IEEE International Symposium on Inertial Sensors and Systems.IEEE,2016:1-4.
[24] Trusov A A,Meyer A D,Mccammon G H,et al.Toward software defined coriolis vibratory gyroscopes with dynamic self-calibration[C]//2016DGON Intertial Sensors and Systems(ISS).IEEE,2016:1-11.
[25] Bryan G H.On the beats in the vibrations of a revolving cylinder or bell[J].Cambridge Philosophical Society,1980,7(3):101.
[26] Rozelle D M,Meyer A D,Trusov A A,et al.MilliHRG inertial sensor assembly-a reality[C]//2015IEEE International Symposium on Inertial Sensors and Systems(ISISS).IEEE,2015:1-4.
[27] Meyer D,Rozelle D.Milli-HRG inertial navigation system[J].Gyroscopy and Navigation,2012,3(4):227-234.
[28] Trusov A A,Phillips M R,Bettadapura A,et al.mHRG:Miniature CVG with beyond navigation grade performance and real time self-calibration[C]//2016 IEEE International Symposium on Inertial Sensors and Systems.IEEE,2016:29-32.
[29] Safran Electronics&Defense.BlueNaute PRIMUS半球谐振惯性系统[DB/OL].[2017-11-10].https://wenku.baidu.com/view/c1dfc81930b765ce-0508763231126edb6e1a767f.html.
[30]上海航天技术研究院半球谐振陀螺组合首飞成功[EB/OL].http://www.360doc.com/content/17/0620/19/28704984_664958132.shtml.
[2] Matthews A,Rybak F J.Comparison of hemispherical resonator gyro and optical gyros[J].Aerospace&Electronic Systems Magazine IEEE,1992,7(5):40-46.
[3] Lynch D,Matthews A,Varty G T.Innovative mechanization to optimize inertial sensors for high or low rate operations[J].Symposium Gyro Techonology,1997,16(9):1-9.
[4] Anon.Northrop Grunnan′s hemispherical resonator GYRO matks 30 million operating hours in space[DB/OL].[2016-01-29].http://news.northropgrumman.com/news/releases/northrp-grumman-s-hemispherical-resonator-gyro-marks-30-million-operatinghours-in-space.
[5]沈博昌,伊国兴,任顺清,等.半球谐振陀螺仪谐振子振动特性的有限元分析[J].中国惯性技术学报,2004,12(6):56-60.
[6]周小刚,汪立新,方针,等.半球谐振陀螺平台调平系统设计及仿真[J].宇航学报,2011,32(3):549-553.
[7]高胜利.半球谐振陀螺的分析与设计[D].哈尔滨:哈尔滨工程大学,2008.
[8]杨倩.基于半球谐振陀螺的惯性导航系统研究[D].哈尔滨:哈尔滨工业大学,2009:16-22.
[9]祁家毅,任顺清,冯士伟,等.半球谐振陀螺仪随机误差分析[J].中国惯性技术学报,2009,17(1):98-101.
[10]高胜利,吴简彤.基于多电极的半球谐振陀螺信号检测[J].哈尔滨工程大学学报,2008,29(5):474-478.
[11]雷霆.半球谐振陀螺控制技术研究[D].重庆:重庆大学,2006.
[12]赵洪波.半球谐振陀螺仪误差机理分析与误差抑制方法研究[D].哈尔滨:哈尔滨工业大学,2013.
[13]倪受东,吴洪涛,嵇海平,等.微型半球陀螺仪的误差源研究[J].传感器与微系统,2007,26(1):30-32.
[14] Remillieux G,Goudon J C,Roberfroid D.Coriolisvibrating gyros for aeronautical applications[R].SAE Technical Paper,2011.
[15] Jeanroy A,Bouvet A,Remillieux G.HRG and marine applications[J].Gyroscopy and Navigation,2014,5(2):67-74.
[16] Rozelle D M.The hemispherical resonator gyro:From wineglass to the planets[C]//Proceedings of19th AAS/AIAA Space Flight Mechanics Meeting.2009:1157-1178.
[17] Remillieux G,Delhaye F.Sagem Coriolis Vibrating Gyros:a vision realized[C]//2014 DGON Inertial Sensors and Systems Symposium(ISS).IEEE,2014:1-13.
[18] Remillieux G,Delhaye F.Sagem Coriolis Vibrating Gyros:a vision realized[C]//2014 DGON Inertial Sensors and Systems Symposium(ISS).IEEE,2014:1-13.
[19] Lenoble A,Rouilleault T.PRIMUS:SWAP-oriented IMUs for multiple applications[C]//2016DGON Intertial Sensors and Systems(ISS).IEEE,2016:1-16.
[20] http://www.northropgrumman.com/Capabilities/SIRU/Documents/Scalable_SIRU_Family.pdf.
[21] Trusov A A,Meyer A D,Mccammon G H,et al.Toward software defined coriolis vibratory gyroscopes with dynamic self-calibration[C]//2016DGON Intertial Sensors and Systems(ISS).IEEE,2016:1-11.
[22] Remillieux G,Delhaye F.Sagem Coriolis Vibrating Gyros:a vision realized[C]//2014 DGON Inertial Sensors and Systems Symposium(ISS).IEEE,2014:1-13.
[23] Jeanroy A,Grosset G,Goudon J C,et al.HRG by Sagem from laboratory to mass production[C]//2016IEEE International Symposium on Inertial Sensors and Systems.IEEE,2016:1-4.
[24] Trusov A A,Meyer A D,Mccammon G H,et al.Toward software defined coriolis vibratory gyroscopes with dynamic self-calibration[C]//2016DGON Intertial Sensors and Systems(ISS).IEEE,2016:1-11.
[25] Bryan G H.On the beats in the vibrations of a revolving cylinder or bell[J].Cambridge Philosophical Society,1980,7(3):101.
[26] Rozelle D M,Meyer A D,Trusov A A,et al.MilliHRG inertial sensor assembly-a reality[C]//2015IEEE International Symposium on Inertial Sensors and Systems(ISISS).IEEE,2015:1-4.
[27] Meyer D,Rozelle D.Milli-HRG inertial navigation system[J].Gyroscopy and Navigation,2012,3(4):227-234.
[28] Trusov A A,Phillips M R,Bettadapura A,et al.mHRG:Miniature CVG with beyond navigation grade performance and real time self-calibration[C]//2016 IEEE International Symposium on Inertial Sensors and Systems.IEEE,2016:29-32.
[29] Safran Electronics&Defense.BlueNaute PRIMUS半球谐振惯性系统[DB/OL].[2017-11-10].https://wenku.baidu.com/view/c1dfc81930b765ce-0508763231126edb6e1a767f.html.
[30]上海航天技术研究院半球谐振陀螺组合首飞成功[EB/OL].http://www.360doc.com/content/17/0620/19/28704984_664958132.shtml.