GNSS/INS深组合技术研究进展与展望

doi:10.7527/S1000-6893.2015.0351

Abstract

Abstract:

With the improvement of the performance requirements of the navigation system in aviation, aerospace and military applications, the GNSS/INS deep integration has gradually become the research focus as it is the deepest way of GNSS/INS integration. This paper has introduced different understandings of the deep integration concept based on the origination and development process of GNSS/INS deep integration. According to the variation of the receiver tracking loops and information processing methods, the deeply integrated navigation system can be classified into three modes, which are scalar tracking-based deep integration, coherent vector tracking-based deep integration and non-coherent vector tracking-based deep integration. The coherent vector tracking-based deep integration mode can be further classified into the cascade and centralized architectures. The features are compared and analyzed respectively by providing architectures of different deep integration modes. The researches of the GPS/INS deep integration research at home and abroad are reviewed and problems in the current research are summarized. Finally the future directions of the GPS/INS deep integration are pointed out according to the practical applications.

Key words: GNSS/INS, integrated navigation, deep integration, architecture, vector-based deep integration, scalar-based deep integration

CLC Number:

V443
TN961

NIU Xiaoji, BAN Yalong, ZHANG Tisheng, LIU Jingnan. Research progress and prospects of GNSS/INS deep integration[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(10): 2895-2908.

References

[1] 艾伦, 金玲, 黄晓瑞. GPS/INS组合导航技术的综述与展望[J]. 数字通信世界, 2011, 2(2):58-61. AI L, JIN L, HUANG X R. Overview and prospect of GPS/INS integrated navigation technology[J]. Digital Communication World, 2011, 2(2):58-61(in Chinese).
[2] 谢钢. GPS原理与接收机设计[M]. 北京:电子工业出版社, 2009:278-281. XIE G. Principles of GPS and receiver design[M]. Beijing:Publishing House of Electronics Industry, 2009:278-281(in Chinese).
[3] KAPLAN E, CHRISTOPHER H. Understanding GPS:Principles and applications[M]. Boston:Artech House, 2005:366-368.
[4] PARKINSON B, POWER S. The origins of GPS[J]. GPS World, 2010, 21(6):1-43.
[5] HEMESATH N B, HUTCHINSON W M. Anti-jamming characteristics of GPS/GDM[C]//Proceedings of 1976 National Telecommunications Conference. 1976:41.6-1-41.6-5.
[6] COX D B. Integration of GPS with inertial navigation systems[J]. Navigation, 1978, 25(2):236-245.
[7] COPPS E M, GEIER G J, FIDLER W C, et al. Optimal processing of GPS signals[J]. Navigation, 1980, 27(3):171-182.
[8] NIELSON J T, SWEARINGEN G W, WITSMEER A J. GPS aided inertial navigation[J]. IEEE Aerospace and Electronic Systems Magazine, 1986, 1(3):20-26.
[9] RITLAND J, SPALDING K. Impact of inertial system quality on GPS-inertial performance in a jamming environment:AIAA-1987-2594[R]. Reston:AIAA, 1987.
[10] SPALDING K J. Advanced GPS-inertial integration concepts:AIAA-1989-3501[R]. Reston:AIAA, 1989.
[11] HOMER W C. An introduction to the GPS guidance package (GGP)[C]//Proceedings of the Fifteenth Biennial Guidance Test Symposium. DTIC, 1991:1-4.
[12] SENFFNER D, SENNOTT J W. Navigation receiver with coupled signal-tracking channels:United States Patent 5343209[P]. 1994-08-30.
[13] SPILKER J J. Fundamentals of signal tracking theory[J]. Progress in Astronautics and Aeronautics, 1996(163):245-327.
[14] PHILLIPS R E, SCHMIDT G T. GPS/INS integration[C]//Proceedings of System Implications and Innovative Applications of Satellite Navigation. 1996:9-1-9-18.
[15] ABBOTT A S, LILLO W E. Global positioning systems and inertial measuring unit ultratight coupling method:United States Patent 6516021[P]. 2003-02-04.
[16] GUSTAFSON D, DOWDLE J. Deeply integrated code tracking:Comparative performance analysis[J]. Proceedings of International Technical Meeting of the Satellite Division of The Institute of Navigation, 2003:2553-2561.
[17] GAUTIER J, PARKINSON B. Using the GPS/INS generalized evaluation tool (GIGET) for the comparison of loosely coupled, tightly coupled and ultra-tightly coupled integrated navigation systems[C]//Proceedings of the 59th Annual Meeting of the Institute of Navigation and CIGTF 22nd Guidance Test Symposium. Manassas, VA:ION, 2003:65-76.
[18] GROVES P D, MATHER C J, MACAULAY A. Demonstration of non-coherent deep INS/GPS integration for optimized signal-to-noise performance[C]//Proceedings of the 20th International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2007:2627-2638.
[19] PETOVELLO M, LACHAPELLE G. Comparison of vector-based software receiver implementations with application to ultra-tight GPS/INS integration[C]//Proceedings of the 19th International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2006:1790-1799.
[20] PETOVELLO M, O'DRISCOLL C, LACHAPELLE G. Ultra-tight GPS/INS for carrier phase positioning in weak-signal environments[C]//Proceedings of NATO RTO SET-104 Symposium on Military Capabilities Enabled Advances in Navigation Sensors. NATO, 2007:1-18.
[21] 高帅和, 赵琳. 不同GPS/SINS超紧组合框架的分析与等价性推导[J]. 中国惯性技术学报, 2011, 10(5):571-574. GAO S H, ZHAO L. Analysis and equivalence derivation of different ultra-tight coupled navigation structures[J]. Journal of Chinese Inertial Technology, 2011, 10(5):571-574(in Chinese).
[22] HWANG D, LIM D W, CHO S L, et al. Unified approach to ultra-tightly-coupled GPS/INS integrated navigation system[J]. IEEE Aerospace and Electronic Systems Magazine, 2011, 26(3):30-38.
[23] 秦永元, 俞济祥. 惯导速度辅助下GPS接收机码环的噪声响应和动态跟踪性能分析[J]. 航空学报, 1990(12):564-569. QIN Y Y, YU J X. Noise response and manoeuver tracking performance analysis for the GPS receiver code loop aided by the INS velocity[J]. Acta Aeronautica et Astronautica Sinica, 1990(12):564-569(in Chinese).
[24] 陈家斌, 袁信. 惯性速度辅助下GPS/捷联惯导组合系统性能研究[J]. 南京航空航天大学学报, 1994, 26(6):730-736. CHEN J B, YUAN X. Research on performance of inertial velocity aiding GPS/SNS integrated system[J]. Journal of Nanjing University of Aeronautics and Astronautics, 1994, 26(6):730-736(in Chinese).
[25] LASHLEY M, BEVLY D M, HUNG J Y. Analysis of deeply integrated and tightly coupled architectures[C]//IEEE/ION 2010 Position, Location and Navigation Symposium. Piscataway, NJ:IEEE Press, 2010:382-396.
[26] GUSTAFSON D E, DOWDLE J R, ELWELL J M. Deeply-integrated adaptive GPS-based navigator with extended-range code tracking:United States Patent 6331835[P]. 2001-12-18.
[27] CRANE R, ALEXANDER S, BESER J, et al. System and method for advanced tight coupling of GPS and inertial navigation sensors:United States Patent 7274504[P]. 2007-09-25.
[28] GEBRE-EGZIABHER D, RAZAVI A, ENGE P, et al. Doppler aided tracking loops for SRGPS integrity monitoring[C]//Proceedings of the 16th International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2003:2562-2571.
[29] CHIOUT Y, GEBRE-EGZIABHER D, WALTER T, et al. Model analysis on the performance for an inertial aided FLL-assisted-PLL carrier-tracking loop in the presence of ionospheric scintillation[C]//Proceedings of the 2007 National Technical Meeting of the Institute of Navigation. Manassas, VA:ION, 2007:2895-2910.
[30] KREYE C, EISSFELLER B, LUCK T. Improvements of GNSS receiver performance using tightly coupled INS measurements[C]//Proceedings of Intl Symposium on Kinematic Systems in Geodesy, Geomatics, and Navigation. 2001:15-25.
[31] ALBAN S, AKOS D, ROCK S. Performance analysis and architectures for INS-aided GPS tracking loops[C]//Proceedings of the 2003 National Technical Meeting of the Institute of Navigation. Manassas, VA:ION, 2003:611-622.
[32] 张提升. GNSS/INS标量深组合跟踪技术与原型系统验证[D]. 武汉:武汉大学, 2013:73-100, 116-121. ZHANG T S. Research on the tracking technology of GNSS/INS deep integration based on hardware prototype[D]. Wuhan:Wuhan University, 2013:73-100, 116-121(in Chinese).
[33] ANDERSON R S, HANSON D S, KOUREPENIS A S. Evolution of low-cost MEMS inertial system technologies[C]//Proceedings of the 14th International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2001:1332-1342.
[34] HEGG J. Enhanced space integrated GPS/INS (SIGI)[J]. Aerospace and Electronic Systems Magazine, 2002, 17(4):26-33.
[35] 于海亮. 基于INS辅助的GPS接收机捕获和跟踪技术研究[D]. 长沙:国防科学技术大学, 2007:61-68. YU H L. Research on the acquisition and tracking technology of INS-aided GPS receiver[D]. Changsha:National University of Defense Technology, 2007:61-68(in Chinese).
[36] 匡鸿博. 高动态GPS信号跟踪技术的研究[D]. 上海:上海交通大学, 2010:49-58. KUANG H B. Research on GPS signal tracking under high dynamic condition[D]. Shanghai:Shanghai Jiao Tong University, 2010:49-58(in Chinese).
[37] WANG Y, CHEN X, CAI J, et al. Design and analysis of high dynamic GPS/SINS integrated navigation schemes[C]//Proceedings of the 2nd International Conference on Intelligent Control and Information Processing. Piscataway, NJ:IEEE Press, 2011:464-466.
[38] HORSLUND J M, HOOKER J R. Increase jamming immunity by optimizing processing gain for GPS/INS systems:United States Patent 5983160[P]. 1999-11-09.
[39] GUSTAFSON D, DOWDEL J, FLUECKIGER K. A high anti-jam GPS-based navigator[C]//IEEE 2000 Position Location and Navigation Symposium. Piscataway, NJ:IEEE Press, 2000:495-503.
[40] KIM J W, HWANG D H, LEE S J. Performance evaluation of INS velocity-aided tracking loop and deeply coupled GPS/INS integration system in jamming environment[C]//Proceedings of the 63rd Annual Meeting of the Institute of Navigation. Manassas, VA:ION, 2007:742-748.
[41] PARK D B, SHIN D H, OH S H, et al. Velocity aiding-based anti-jamming method for GPS adaptor kits[J]. Transactions of the Japan Society for Aeronautical and Space Sciences, 2011, 54(184):130-136.
[42] JOVANCEVIC A, BROWN A, GANGULY S, et al. Ultra tight coupling implementation using real time software receiver[C]//Proceedings of the 17th International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2004:1575-1586.
[43] 唐康华. GPS/MIMU嵌入式组合导航关键技术研究[D]. 长沙:国防科学技术大学, 2008:71-75. TANG K H. Research on the key technology of embedded GPS/MIMU integrated navigation[D]. Changsha:National University of Defense Technology, 2008:71-75(in Chinese).
[44] 陈坡, 孙付平, 郝万亮, 等. GNSS/INS深组合导航系统性能分析[C]//2012年中国卫星导航学术年会. 广州:中国学术期刊电子出版社, 2012:1-6. CHEN P, SUN F P, HAO W L, et al. Performance analysis of deep integrated GNSS/INS system[C]//Proceedings of CSNC 2012. Guangzhou:China Academic Journal Electronic Publishing House, 2012:1-6(in Chinese).
[45] SOLOVOEV A, GUNAWARDENA S, VAN GRAAS F. Deeply integrated GPS/low-cost IMU for low CNR signal processing:Flight test results and real time implementation[C]//Proceedings of the 17th International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2004:1598-1608.
[46] SOLOVOEV A, BRUCKNER D, VAN GRAAS F, et al. Assessment of GPS signal quality in urban environments using deeply integrated GPS/IMU[C]//Proceedings of the 2007 National Technical Meeting of the Institute of Navigation. Manassas, VA:ION, 2007:815-828.
[47] SOLOVOEV A, GUNAWARDENA S, VAN GRAAS F. Deeply integrated GPS/low-cost IMU for low CNR signal processing:Concept description and in-flight demonstration[J]. Navigation, 2008, 55(1):1-13.
[48] GAO G, LACHPELLE G. INS-assisted high sensitivity GPS receivers for degraded signal navigation[C]//Proceedings of the 19th International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2006:2977-2989.
[49] PETOVELLO M, O'DRISCOLL C, LACHPELLE G. Carrier phase tracking of weak signals using different receiver architectures[C]//Proceedings of the 2008 National Technical Meeting of the Institute of Navigation. Manassas, VA:ION, 2008:28-30.
[50] CHIOU T Y, SEO J, WALTER T, et al. Performance of a Doppler-aided GPS navigation system for aviation applications under ionospheric scintillation[C]//Proceedings of the 21st International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2008:1139-1147.
[51] PANY T, WINKE J, RIEDL B, et al. Performance of a partially coherent ultra-tightly coupled GNSS/INS pedestrian navigation system enabling coherent integration times of several seconds to track GNSS signal down to 1.5 dB-Hz[C]//Proceedings of the 22nd International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2009:2225.
[52] SOLOVOEV A, DICKMAN T J. Deeply integrated GPS for indoor navigation[C]//Proceedings of 2010 International Conference on Indoor Positioning and Indoor Navigation (IPIN). Piscataway, NJ:IEEE Press, 2010:1-9.
[53] 赵琳, 赵洪斌, 闫超. 复杂环境下INS辅助GPS跟踪环路研究[J]. 传感器与微系统, 2011, 10(10):22-25. ZHAO L, ZHAO H B, YAN C. Study on tracking loops of INS-aided GPS in complex environment[J]. Transducer and Microsystem Technologies, 2011, 10(10):22-25(in Chinese).
[54] WANG X, JI X, FENG S. A scheme for weak GPS signal acquisition aided by SINS information[J]. GPS Solutions, 2013, 18(2):243-252.
[55] CHIOU T Y, ALBAN S, ATWATER S, et al. Performance analysis and experimental validation of a Doppler-aided GPS/INS receiver for JPALS applications[C]//Proceedings of the 17th International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2004:1609-1618.
[56] WATSON R, PETOVELLO M, LACHAPELLE, et al. Impact of oscillator errors on IMU-Aided GPS tracking loop performance[C]//Proceedings of European Navigation Conference GNSS. Geneva:ENC, 2007:2931-1-15.
[57] KIESEL S, LANGER M, ECKERT M, et al. Discriminator weighting and performance of a deeply coupled GPS/INS system at low CN0[C]//Proceedings of the 2011 International Technical Meeting of the Institute of Navigation. Manassas, VA:ION, 2001:858-867.
[58] TSUJⅡ T, FUJIWARA T, SUGANUMA Y, et al. Development of INS-aided GPS tracking loop and flight test evaluation[J]. SICE Journal of Control, Measurement, and System Integration, 2011, 4(1):15-21.
[59] BAN Y, NIU X, ZHANG T, et al. Low-end MEMS IMU can contribute in GPS/INS deep integration[C]//IEEE/ION Position, Location and Navigation Symposium. Piscataway, NJ:IEEE Press, 2014:746-752.
[60] HYSLOP G, GERTH D, KRAEMER J. GPS/INS integration on the standoff land attack missile (SLAM)[C]//IEEE Position Location and Navigation Symposium. Piscataway, NJ:IEEE Press, 1990:407-412.
[61] SHERMAN P, HOLMES S. Personal navigation systems:TR-6/004[R]. DTIC, 2005.
[62] Northrop Grumman, LN251 Datasheet[EB/OL]. (2013)
[2015] .http://www.northropgrumman.com/Capabilities/LN251INSGPS/Documents/ln251.pdf.
[63] Northrop Grumman, LN251 Datasheet[EB/OL]. (2013)
[2015] .http://www.northropgrumman.com/Capabilities/LN270PLANS/Documents/ln270.pdf.
[64] BUCK T M, WILMOT J, COOK M J. A high G, MEMS based, deeply integrated, INS/GPS, guidance, navigation and control flight management unit[C]//Proceedings of IEEE/ION Plans. Piscataway, NJ:IEEE Press, 2006:772-794.
[65] KVH, CNS-5000[EB/OL].http://www.kvh.com/Press-Room/Press-Release-Library/2008/080507-CNS5000-Intro.aspx.
[66] UTC-AEROSPACE-SYSTEM, SiNAV[EB/OL]. (2014)
[2015] .http://utcaerospacesystems.com/Pages/Default.aspx.
[67] GAUTIER J D. GPS/INS generalized evaluation tool (GIGET) for the design and testing of integrated navigation systems[D]. Stanford, California:Stanford University, 2003:29-39.
[68] DYRUD L, WOESSNER B, JOVANCEVIC A, et al. Ultra-tightly coupled GPS/INS receiver for TSPI applications[C]//Proceedings of the 20th International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2007:2564-2572.
[69] LI T, GEORGY J, SYED Z, et al. Real-time navigation system for ultra-tight integration of GNSS and multi-sensors[C]//Proceedings of the 26th International Technical Meeting of the ION Satellite Division. Manassas, VA:ION, 2013:2269-2275.
[70] LI T, PETOVELLO M G, LACHAPELLE G, et al. Performance evaluation of ultra-tight integration of GPS/vehicle sensors for land vehicle navigation[C]//Proceedings of the 21st International Technical Meeting of the Satellite Division of the Institute of Navigation. Manassas, VA:ION, 2009:22-25.
[71] LI T, PETOVELLO M, LACHAPELLE G, et al. Real-time ultra-tight integration of GPS L1/L2C and vehicle sensors[C]//Proceedings of the 2011 International Technical Meeting of the Institute of Navigation. Manassas, VA:ION, 2011:2426.
[72] BUSING H G, HAAK U, HECKER P. Aiding GNSS signal tracking loops using vehicle dead reckoning sensors[C]//Proceedings of the 2013 International Technical Meeting of the Institute of Navigation. Manassas, VA:ION, 2013.
[73] FERNANDEZ A, DIEZ J, DE CASTRO D, et al. ATENEA:Advanced techniques for deeply integrated GNSS/INS/LiDAR navigation[C]//20105th ESA Workshop on Satellite Navigation Technologies and European Workshop on GNSS Signals and Signal Processing (NAVITEC). Piscataway, NJ:IEEE Press, 2010:1-8.
[74] LANGER M, KIESEL S, ASCHER C, et al. Deeply coupled GPS/INS integration in pedestrian navigation systems in weak signal conditions[C]//2012 International Conference on Indoor Positioning and Indoor Navigation (IPIN). Piscataway, NJ:IEEE Press, 2012:1-7.

Research progress and prospects of GNSS/INS deep integration

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