精密着舰导航是提升航空母舰作战效能的重要保障。高精度的载波相位差分定完好性监测方法是满足精密着舰导航高精度和高可靠性的必然选择。考虑到影响精密着舰导航精度及可靠性的多重风险源，重点针对保证着舰可靠性的完好性监测法，分别从完好性风险概率分配技术、整周模糊度解算正确性检验以及基线形变量监测等国内外研究现状进行分析和研究，从而为构建精密着舰导航系统的完好性监测技术提供参考和依据。
Precise navigation of ship-landing is the fundamental technology to guarantee the fighting efficiency improvement of aircraft-carrier. The integrity monitoring methodology of high-precision carrier-phase differential positioning is the inevitable choice to satisfying the demanding navigational requirements of high accuracy and high reliability. Regarding to the effect of multiple integrity risk resources on navigation accuracy and reliability of precise ship-landing, we focus on the integrity monitoring methods for the reliability of precise ship-landing by the analyzing and summarizing the technologies of integrity risk probability allocation, the correctness validation of integer ambiguity, and the baseline flexure detection, which aims to provide the reference and the foundation for the integrity monitoring of precise ship-landing.
2018,40(7): 121-124,132 收稿日期：2018-04-10
DOI：10.3404/j.issn.1672-7649.2018.07.022
分类号：U666.1
基金项目：国家自然科学基金重点资助项目（61773132）；国家自然科学基金面上资助项目（61633008）；工信部创新专项资助项目；中央高校基金基本科研业务费资助项目（HEUCFP201768）；黑龙江省博士后科研启动基金资助项目（LBH-Q15033）
作者简介：陈晶(1966-),女,高级工程师,研究方向为卫星导航
参考文献：
[1] LI Jie, YU Chuan. The equipment for aircraft landing of aircraft carrier[J]. Modern Millitary, 2006, (10):56-58.
[2] HUANG Z, HUANG Z, ZHU Y. A New Optimal Hatch Filter to Minimize the Effects of Ionosphere Gradients for GBAS[J]. Chinese Journal of Aeronautics, 2008, 21(6):526-532.
[3] RIFE J, KHANAFSEH S, PULLEN S, et al. Navigation, Interference Suppression, and Fault Monitoring in the Sea-Based Joint Precision Approach and Landing System[J]. Proceedings of the IEEE, 2009, 96(12):1958-1975.
[4] YANG Tei-jun. The study on the GPS based real-time attitude determination technique and multipath effects[D]. University of Electronic Science and Technology, 2003.
[5] ZHOU Yang-mei, LIU Jing-nan. Rigor method on evaluating the rightness for the integer solution of GPS carried-phase ambiguity[J]. Geomatics and Information Science of Wuhan University, 2004(11):1004-1007.
[6] LACHAPELLE G, SUN H, CANNON M E. Precise aircraft to aircraft positioning using a multiple receiver configuration[C]//Proceedings of the 1994 National Technical Meeting of The Institute of Navigation, San Diego, CA, January 1994, 793-799.
[7] GEBRE-EGZIABHER D, SHAO Y. Model for JPALS/SRGPS flexure and attitude error allocation[J]. IEEE Transactions on Aerospace & Electronic Systems, 2015, 46(2):483-495.
[8] XIE Shijie, ZHONG shao long. On Multipath Error of GPS Phase Measurements[J]A Chinese Journal of Cancer Research, 2003, (5):1-5.
[9] RIFE J H, PULLEN S P. The Impact of Measurement Biases on Availability for Category Ⅲ LAAS[J]. Navigation, 2005, 52(4):215-228.
[10] PERVAN B, PULLEN S, SAYIM I. Sigma estimation, inflation, and monitoring in the LAAS ground system[C]//Proceedings of the 13th International Technical Meeting of the satellite division of the institute of navigation (ION GPS 2000), Salt Lake City, UT, September 2000:1234-1244.
[11] TEUNISSEN P J G, VERHAGEN S. GNSS Carrier phase ambiguity resolution:challenges and open problems[M]//Observing our Changing Earth. Springer Berlin Heidelberg, 2009:785-792.
[12] TEUNISSEN P J G, KLEUSBERG A. GPS for Geodesy[J]. Springer Berlin, 1998, 60:271-318.
[13] TEUNISSEN P J G. Mixed Integer Estimation and Validation for next generation GNSS[M]. Springer Berlin Heidelberg, 2015.
[14] WANG Guiwen, WANG Zhemin. Probabilistic properties of GNSS integer ambiguity[J]. Journal of Liaoning Technical University, 2007, 26(4):497-500.
[15] WANG Yan, WU Jicang. A Estimation Method for Integer Parameter Reliability in GPS[J]. Journal of Geodesy and Geodynamics, 2009, 29(5):103-106.
[16] VERHAGEN S. The GNSS Integer Ambiguities:Estimation and Validation[J]. Aerospace Engineering, 2005.
[17] HENKEL P, GÜNTHER C. Reliable Integer Ambiguity Resolution:Multi-Frequency Code Carrier Linear Combinations and Statistical A Priori Knowledge of Attitude[J]. Navigation, 2012, 59(1):61-75.
[18] JI S, CHEN W, DING X, et al. Ambiguity validation with combined ratio test and ellipsoidal integer aperture estimator. J Geodesy[J]. Journal of Geodesy, 2010, 84(10):597-604.
[19] ZHANG Qin, CHEN Yongqi. Validity test based on the probability characteristic of the Integer[J]. Science of Surveying and Mapping, 2003, 28(2):16-19.
[20] FENG S, OCHIENG W, SAMSON J, et al. Integrity Monitoring for Carrier Phase Ambiguities[J]. Journal of Navigation, 2012, 65(1):41-58.
[21] 李亮. 陆基增强系统定位与完好性监测技术研究[D]. 哈尔滨:哈尔滨工程大学, 2012.
[22] TANG H, PULLEN S, ENGE P, et al. Ephemeris type a fault analysis and mitigation for LAAS[C]//Position Location and Navigation Symposium. IEEE, 2010:654-666.
[23] LI L, QUDDUS M, ISON S, ZHAO L. Multiple reference consistency check for LAAS:a novel position domain approach[J]. Gps Solutions, 2012, 16(2):209-220.
[24] AHN I, BRESLAU R, SENNOTT J. Development and evaluation of a precision coordinate transfer system for SRGPS[C]//ION GNSS 17th International Technical Meeting of the Satellite Division, 2004, 1277-1287.
