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车载GNSS失锁下基于BPNN的微陀螺误差估计及定位方法研究 被引量:1

Research on error estimation of micro-gyroscope and location method based on BPNN for vehicle during GNSS outages
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摘要 针对在全球导航卫星系统(global navigation satellite system,GNSS)失锁阶段将微陀螺惯性系统作为备用定位系统时,由于微陀螺误差引起的定位误差发散问题,提出了基于后向传播神经网络(back propagation neural network,BPNN)的微陀螺误差估计及定位算法。在GNSS有效阶段为车辆提供定位信息,同时对微陀螺误差进行估计,并利用后向传播神经网络BPNN建立微陀螺误差预测模型,为GNSS失锁阶段车辆定位做准备;在GNSS失锁阶段,利用已建立好的微陀螺误差预测模型估计微陀螺误差,对微陀螺输出信息进行补偿,以抑制由陀螺误差引起的定位误差。最后利用仿真与试验验证了此方法的正确性与有效性。 In the global navigation satellite system(GNSS)outages phase,the micro-gyroscope inertial system is used as a standby positioning system.In order to solve the problem of positioning divergence error caused by micro-gyroscope error,the error estimation of the micro-gyroscope and location method based on back propagation neural network(BPNN)is proposed in this paper.In the GNSS effective phase,it provides positioning information for vehicles and estimates the micro-gyroscope error.A prediction model of micro-gyroscope error that is prepared for vehicle positioning in the GNSS outages phase is established by the BPNN.In the GNSS outages phase,the micro-gyroscope error prediction model is used to estimate the micro-gyroscope error and compensate the output information of the micro-gyroscope to suppress the positioning error caused by the gyroscope error.Finally,the correctness and effectiveness of this method is verified by simulation and experiment.
作者 王秋滢 刘凯悦 尹娟 WANG Qiuying;LIU Kaiyue;YIN Juan(College of Information and Communication Engineering, Harbin Engineering University, Harbin 150001, China)
出处 《系统工程与电子技术》 EI CSCD 北大核心 2020年第5期1139-1145,共7页 Systems Engineering and Electronics
基金 国家自然科学基金(51879046) 黑龙江省自然科学基金优秀青年项目(YQ2019F001)资助课题。
关键词 全球导航卫星系统失锁 微陀螺惯性系统 微陀螺误差 预测 global navigation satellite system(GNSS)outages micro-gyroscope inertial system micro-gyroscope error prediction
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  • 1Jan Wendel, Oliver Meister, Christian Schlaile, GertF Trommer. An integrated GPS/MEMS - IMU navigation system[J]. Aerospace Science and Technology, May,2006.
  • 2Helen Basikl, M R Ananthasayanam, S N Purl. Adaptive Kalman Filter Tuning In Integration of Low - Cost MEMS - INS/GPS[ C ]. Guidan, Navigation, and Control Conference and Exhibit, August, 2004.
  • 3S Winkler, M Buschmann, T Kordes, H W Schulz, P Vorsmann. Application of Micro - Technology to Integrated Navigation of Autonomous Micro Air Vehicles [ C ]. Conference on Micro - Nano - Technologies, November 2004.
  • 4STAUFFER J M, et al. RS9000 a novel MEMS acceierometer family for mil/aerospace and safety critical applications [ M ]. IEEE/ION PLANS, Indian Wells ,CA ,2010.
  • 5DONG Y,et al. High performance inertial navigation grade sigma-delta MEMS accelerometer [M].IEEE PLANS, Indian Wells, CA,2010.
  • 6LIU C. KENNY T. A high-precision,wide-bandwidth micro- machined tunneling accelerometer [ J ]. IEEE Journal of Microelectromechanical Systems ( ISSN 1057 - 7157 ) , 2001,10(3) :425 -433.
  • 7DONG H, et al. A novel out-of-plane MEMS tunneling accelerometer with excellent Low frequency resolution [ M ]. 1st IEEE International Conference on Nano/Micro Engineered and Molecular Systems,Zhuhai, China,2006.
  • 8LE TRAON O,et al. The DIVA accelerometer and VIG gyro: two quartz inertial MEMS for guidance and navigation applications [ M ]. IEEE/ION PLANS, Indian Wells, CA ,2010.
  • 9HOPKINS R, et al. The silicon oscillating accelerometer:a high-performance MEMS accelerometer for precision navigation and strategic guidance applications, ION 61st Annual Meeting, Cambridge, MA ,2005.
  • 10BECKA S,et al. A high reliability solid-state accelerometer for ballistic missile inertial guidance, AIAA GN&C, Honolulu, HI ,2008.

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