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-  2018 

车载三天线GNSS的直接法定姿及精度评估
Direct Attitude Determination Method Based on Vehicle-mounted Three-antenna GNSS and the Accuracy Evaluation

DOI: 10.13203/j.whugis20160171

Keywords: 直接法,动态定姿,基线,多值性问题,精度,可靠性,
direct method
,dynamic attitude determination,baseline,multi-value problem,accuracy,reliability

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Abstract:

针对移动测量系统对载体姿态的需求,对车载三天线全球卫星导航系统(global navigation satellite system,GNSS)的直接法定姿进行了研究。分析了定姿的原理,给出了姿态解算公式,并提出一种简便的方法确定航向角的象限,解决了航向角的多值性问题。为了评估该方法的精度,利用车载的三天线GNSS进行了动态实验,采集了动态观测数据,利用直接法对观测数据进行了姿态解算,并用同车搭载的一套高精度惯性导航系统(inertial navigation system,INS)给出的姿态参考值对三天线GNSS定姿的精度和可靠性进行了评估。结果表明,三天线GNSS直接法定姿精度高、可靠性好,并具有计算简便,可避免奇异性问题等优点

References

[1]  Liu S, Sun F, Zhang L, et al. Tight Integration of Ambiguity-fixed PPP and INS:Model Description and Initial Results[J]. <em>GPS Solutions</em>, 2016, 20(1):39-49
[2]  Rabbou M A, El-Rabbany A. Tightly Coupled Integration of GPS Precise Point Positioning and MEMS-based Inertial Systems[J]. <em>GPS Solutions</em>, 2015, 19(4):601-609
[3]  Wu Z, Yao M, Ma H, et al. Low-cost Attitude Estimation with MIMU and Two-antenna GPS for Satcom-on-the-Move[J]. <em>GPS Solutions</em>, 2013, 17(1):75-87
[4]  Aleshechkin A. Algorithm of GNSS-based Attitude Determination[J]. <em>Gyroscopy and Navigation</em>, 2011, 2(4):269-276
[5]  Ballal T, Bleakley C J. GNSS Instantaneous Ambiguity Resolution and Attitude Determination Exploiting the Receiver Antenna Configuration[J]. <em>IEEE Transactions on Aerospace and Electronic Systems, 2014, 50(3):2061-2069</em>
[6]  Qu Jianming, Qin Honglei, Jin Tian, et al. Improved Attitude Determination Technique of GNSS Based on Baseline Constraint and Recursive Multiple-epoch[J]. <em>Journal of PLA University of Science and Technology (Natural Science Edition)</em>, 2014, 15(5):428-433(曲建铭, 秦红磊, 金天, 等. 基于基线约束及递推多历元的改进GNSS定姿技术[J]. 解放军理工大学学报(自然科学版), 2014, 15(5):428-433)
[7]  Madeira S, Gon?alves J, Bastos L. Accurate DTM Generation in Sand Beaches Using Mobile Mapping[J]. <em>Journal of Coastal Conservation</em>, 2013, 17(3):579-588
[8]  Wu Fumei, Nie Jianliang, He Zhengbin. Low-cost GPS/INS Integrated Navigation Algorithm in Land Vehicle System Considering Attitude Update[J].<em>Journal of Chinese Inertial Technology</em>, 2010, 18(6):675-679(吴富梅, 聂建亮, 何正斌. 低成本车载GPS/INS组合导航姿态角更新算法[J].中国惯性技术学报, 2010, 18(6):675-679)
[9]  Hide C, Pinchin J, Park D. Development of a Low Cost Multiple GPS Antenna Attitude System[C]. The 20th International Technical Meeting of the Satellite Division of The Institute of Navigation, Manassas, VA, 2007
[10]  Liu Genyou, Ou Jikun. Determining Attitude with Single Epoch GPS Algorithm and Its Precision Ana-lysis[J]. <em>Geomatics and Information Science of Wuhan University</em>, 2003, 28(6):732-735(刘根友,欧吉坤. GPS单历元定向和测姿算法及其精度分析[J]. 武汉大学学报·信息科学版, 2003, 28(6):732-735)
[11]  Kukko A, Kaartinen H, Hyypp? J, et al. Multiplatform Mobile Laser Scanning:Usability and Performance[J]. <em>Sensors</em>, 2012, 12(9):11712-11733
[12]  Li Y, Efatmaneshnik M, Dempster A. Attitude Determination by Integration of MEMS Inertial Sensors and GPS for Autonomous Agriculture Applications[J]. <em>GPS Solutions</em>, 2012, 16(1):41-52
[13]  Teunissen P J G. The Affine Constrained GNSS Attitude Model and Its Multivariate Integer Least-squares Solution[J]. <em>Journal of Geodesy</em>, 2012, 86(7):547-563
[14]  Tenn H K, Jan S S, Hsiao F B. Pitch and Roll Attitude Estimation of a Small-scaled Helicopter Using Single Antenna GPS with Gyroscopes[J]. <em>GPS Solutions</em>, 2009, 13(3):209-220
[15]  Axelrad P, Ward L M. Spacecraft Attitude Estimation Using the Global Positioning System:Metho-dology and Results for RADCAL[J]. <em>Journal of Guidance, Control and Dynamics</em>, 1996, 19(6):1201-1209
[16]  Chen W, Qin H. New Method for Single Epoch, Single Frequency Land Vehicle Attitude Determination Using Low-end GPS Receiver[J]. <em>GPS Solutions</em>, 2012, 16(3):329-338
[17]  Wang Y, Zhang X, Zhang Y. Improved Ambiguity Function Method Based on Analytical Resolution for GPS Attitude Determination[J]. <em>Measurement Science and Technology</em>, 2007, 18(9):2986-2990
[18]  Lu G. Development of a GPS Multi-antenna System for Attitude Determination[D]. Calgary:University of Calgary, 1995
[19]  He Haibo. Precise Kinematic GPS Surveying and Quality Control[D]. Zhengzhou:Information Engineering University, 2002(何海波. 高精度GPS动态测量及质量控制[D].郑州:信息工程大学, 2002)
[20]  Wang Bing, Sui Lifen, Zhang Qinghua, et al. Research on Attitude Determination Algorithms Using GPS[J]. <em>Geomatics and Information Science of Wuhan University</em>, 2013, 38(12):1392-1395(王冰, 隋立芬, 张清华, 等. 利用GPS解算载体测姿的算法研究[J]. 武汉大学学报·信息科学版, 2013, 38(12):1392-1395)
[21]  Qin Yongyuan. Inertial Navigation[M]. Beijing:Science Press, 2006(秦永元. 惯性导航[M]. 北京:科学出版社, 2006)

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