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电缆长度辅助的光纤陀螺测斜仪组合测量方法

张春熹 林铁 王璐 李先慕 徐美宝

张春熹, 林铁, 王璐, 等 . 电缆长度辅助的光纤陀螺测斜仪组合测量方法[J]. 北京航空航天大学学报, 2015, 41(5): 764-769. doi: 10.13700/j.bh.1001-5965.2014.0382
引用本文: 张春熹, 林铁, 王璐, 等 . 电缆长度辅助的光纤陀螺测斜仪组合测量方法[J]. 北京航空航天大学学报, 2015, 41(5): 764-769. doi: 10.13700/j.bh.1001-5965.2014.0382
ZHANG Chunxi, LIN Tie, WANG Lu, et al. Integrated surveying method for FOG inclinometer aided by cable length[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 764-769. doi: 10.13700/j.bh.1001-5965.2014.0382(in Chinese)
Citation: ZHANG Chunxi, LIN Tie, WANG Lu, et al. Integrated surveying method for FOG inclinometer aided by cable length[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 764-769. doi: 10.13700/j.bh.1001-5965.2014.0382(in Chinese)

电缆长度辅助的光纤陀螺测斜仪组合测量方法

doi: 10.13700/j.bh.1001-5965.2014.0382
详细信息
    通讯作者:

    张春熹(1965—),男,湖南岳阳人,教授,zhangchunxi@buaa.edu.cn,主要研究方向为惯性导航技术、光纤陀螺及信号检测等.

  • 中图分类号: TE927+.6

Integrated surveying method for FOG inclinometer aided by cable length

  • 摘要: 为实现光纤陀螺(FOG)测斜仪高精度长时间测量,结合测井作业方式,提出基于卡尔曼滤波技术的电缆长度信息辅助的组合测量方法.介绍了捷联惯性测量系统(ISS)误差模型和电缆长度测量模型,设计了组合测量方法的总体方案,建立了组合测量系统误差状态模型及量测更新模型.采用半实物仿真计算对本文提出的组合测量方法进行了验证.仿真结果表明:14 400 s的仿真过程,井斜角误差小于0.02°,工具面角误差小于0.12°,方位角误差小于0.98°,位置误差小于47.5 m.相比纯惯性测量,误差得到了有效的抑制,保证了仪器长时间保精度的测量,提高了仪器的性能.

     

  • [1] Noureldin A.New measurement-while-drilling surveying technique utilizingsets of fiber optic rotation sensors[D].Calgary:University of Calgary,2002.
    [2] Torkildsen T,Edvardsen I,Fjogstad A,et al.Drilling fluid affects MWD magnetic azimuth and wellbore position[C]//Proceedings of IADC/SPE Drilling Conference.Dallas,Texas:SPE,2004:595-602.
    [3] Ledroz A G,Pecht E,Cramer D,et al.FOG-based navigation in downhole environment during horizontal drilling utilizing a complete inertial measurement unit:directional measurement-while-drilling surveying[J].IEEE Transations on Instrumentation and Measurement,2005,54(5):1997-2006.
    [4] ElGizawy M L.Continuous measurement while drilling surveying system utilizing MEMS inertial sensors[D].Calgary:University of Calgary,2009.
    [5] Noureldin A,Tabler H,Irvine-Halliday D,et al.Testing the applicability of fiber optic gyroscopes for azimuth monitoring for measurement-while-drilling processes in the oil industry[C]//Proceedings of IEEE Symposium on Position Location and Navigation.Piscataway,NJ:IEEE,2000:291-298.
    [6] 张春熹,高爽.自主式光纤陀螺油井测斜仪[J].仪表技术与传感器,2006(11):9-11. Zhang C X,Gao S.Autonomous fiber optic gyroscopes inclinometer for well logging[J].Instrument Technique and Sensor,2006(11):9-11(in Chinese).
    [7] 颜廷洋,张春熹,高爽,等.光纤陀螺测斜仪设计和实验[J].中国惯性技术学报,2013,21(2):179-181. Yan T Y,Zhang C X,Gao S,et al.Design and experiments of FOG inclinometer for surveying borehole[J].Journal of Chinese Inertial Technology,2013,21(2):179-181(in Chinese).
    [8] Zhang Y S,Wang S W,Fang J C.Measurement while drilling instrument based on predigested inertial measurement unit[J].IEEE Transations on Instrumentation and Measurement,2012,61(12): 3295-3302.
    [9] 颜廷洋,张春熹,高爽,等.附加运动约束的光纤陀螺测斜仪动态测量[J].中国惯性技术学报,2012,20(6):650-653 Yan T Y,Zhang C X,Gao S,et al.Continuous measurement for fiber optic gyro inclinometer with motion constraint[J].Journal of Chinese Inertial Technology,2012,20(6):650-653(in Chinese).
    [10] Shin E H.Estimation techniques for low cost inertial navigation[D].Calgary:University of Calgary,2005.
    [11] Guo J C.Development of a precise GPS/INS/on-board vehicle sensors integrated vehicular positioning system[D].Calgary:University of Calgary,2007.
    [12] Li T.Use of wheel speed sensor to enhance a reduced IMU ultra-tight GNSS receiver[D].Calgary:University of Calgary,2009.
    [13] 林铁,林恒,高爽,等.光纤陀螺测斜仪数据采集及传输单元设计与实现[J].测井技术,2009,33(4):402-405. Lin T,Lin H,Gao S,et al.Design and implementation of data acquisition and transmission for fiber optic gyroscopes inclinometer[J].Well Logging Technology,2009,33(4):402-405(in Chinese).
    [14] Rogers R M.Velocity error reresentations in inertial navigation system error models,AIAA-1995-3193-CP[R].Reston:AIAA,1995.
    [15] Rogers R M.Applied mathematics in integrated navigation systems[M].2nd ed.Reston:American Institute of Aeronautics and Astronautics,2003:77-84.
    [16] 张小跃,杨功流,张春熹.捷联惯导/里程计组合导航方法[J].北京航空航天大学学报,2013,39(7):292-296. Zhang X Y,Yang G L,Zhang C X.Integrated navigation method for SINS and odometer[J].Journal of Beijing University of Aeronautics and Astronautics,2013,39(7):292-296(in Chinese).
    [17] 秦永元,张洪钺,汪叔华.卡尔曼滤波与组合导航原理[M].西安:西北工业大学出版社,1998:69-76. Qin Y Y,Zhang H Y,Wang S H.Theory of Kalman filter and integrated navigation[M].Xi'an:Northwestern Polytechnical University Press,1998:69-76(in Chinese).

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出版历程
  • 收稿日期:  2014-06-25
  • 修回日期:  2014-08-05
  • 刊出日期:  2015-05-20

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