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基于GPS软件接收机的SINS/GPS紧组合系统仿真 被引量:1

Simulation of the Tightly-Coupled SINS/GPS Based on a GPS Software Receiver
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摘要 为了系统验证SINS/GPS紧组合系统的性能,基于GPS软件接收机,进行了仿真系统构建。仿真系统由轨迹发生器、GPS中频信号模拟器、IMU信号模拟器、GPS软件接收机、SINS导航解算模块、组合滤波算法和导航性能分析模块等部分构成,其中详细设计了GPS软件接收机中的捕获和跟踪算法、SINS解算以及基于伪距和伪距率的组合滤波算法。仿真结果表明:紧组合导航系统收敛性较好,能够一定程度上抑制惯导系统误差的积累,有较好的导航性能。设计的该系统满足紧组合导航系统性能验证的需要,也为后续的超紧组合研究奠定了良好的基础。 In order to systematically verify the performance of SINS/GPS tightly-coupled system, based on a GPS software receiver, and a simulation system is constructed. The sim- ulation system consists of a trajectory generator, a GPS IF signal simulator, an IMU signal simulator, a GPS software receiver, a SINS navigation solver module, a Kalman filter, a navigation performance analysis module and other components. The detailed design of the ac- quisition and tracking algorithm of GPS software receiver, SINS solution and Kalman filter based on pseudorange and pseudorange rate is provided. The simulation results show that, tightly-coupled integrated navigation system has a better convergence, can control accumula- ted errors of SINS from a certain extent, so it has a better navigation performance. And the system can meet the needs of tightly-coupled integrated navigation system performance veri- fication. The simulation platform can also be employed for the following research on ultra- tightly-coupled SINS/GPS.
出处 《全球定位系统》 2013年第5期27-33,39,共8页 Gnss World of China
基金 国家航空科学基金(批准号:20100851017)
关键词 SINS GPS软件接收机 紧组合 KALMAN滤波 SINS GPS software receiver tightly-coupled Kalman filter
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参考文献9

  • 1许刚,黄国荣,彭兴钊,薛冬,高圆.GPS软件接收机相关技术研究[J].导弹与航天运载技术,2012(4):45-49. 被引量:4
  • 2LEDVINA B M,DOWELL S P,KINTNER P M,et al. A twelve-channel real-time GPS L1 software re- ceiver[C]//Proceedings of the institute of navigation on national technical meeting,2003:767-782.
  • 3全鹏,朱桂斌,叶久志,孙奥.基于GPS单频软件接收机的捕获与跟踪算法实现[J].全球定位系统,2011,36(5):22-25. 被引量:1
  • 4董绪荣,张守信,华仲春.GPS/INS组合导航定位及其应用[M].长沙:国防科技大学出版社,1987.
  • 5RANK K. GPS and differential GPS: an error model for sensor simulation[C]// Proceedings of IEEE PLANS ,1994: 260 266.
  • 6张浩.SINS/GPS组合导航系统滤波算法研究及工程实现[D].南京:南京理工大学,2008.
  • 7EVANS C D,RIGGINS R. The design and analysis if integrated navigation systems using real INS and GPS data[C]// Proceedings of the IEEE. ]995 NEACON.
  • 8秦永元,张洪钺,汪淑华.卡尔曼滤波与组合导航原理[M].陕西:西北工业大学出版社,2007:33-35,161-165.
  • 9林敏敏,房建成,高国江.GPS/SINS组合导航系统混合校正卡尔曼滤波方法[J].中国惯性技术学报,2003,11(3):29-33. 被引量:17

二级参考文献18

  • 1杨小牛,楼才一,徐建良.软件无线电原理与应用[M].北京:电子工业出版社,2006,2-5.
  • 2谢刚.GPS原理与接收机设计[M].北京:电子工业出版社.2009.
  • 3James Bao-yen T. Fundamentals of global positioning system receivers a software approach [M]. 2nd ed. New York: John Wiley & Sons Inc. , 2007.
  • 4Ledvina B M, Dowell S P, Kintner P M, et al. A twelve-channel real-time GPS L1 software receiver [C]// Proceedings of the institute of navigation on national technical meeting. Anaheim, CA, 2003: 767-782.
  • 5Kaplan, E D. Understanding GPS~ Principles and applications [M]. 2nd ed. MA.. Artech HousePub- lishers, 2007 : 125-130.
  • 6Krunvieda K, Medhani P, Cloman C, et al. A com- plete IF software GPS receiver., a tutorial about the detail [C] // ION GPS 2001, Salt Lake City, UT, 2001 :89-829.
  • 7Upadhyay T. Autonomous GPS/SINS navigation experiment for space transfer vehicle[J]. IEEE Trans on AES. 1993, 29(3):772-784.
  • 8Rank K. GPS and Differential GPS: an error model for sensor simulation[A]. Proceedings of IEEE PLANS 1994[C]. Las Vegas, Nevada. 1994: 260-266.
  • 9杨东凯,张飞舟.软件定义的GPS和伽利略接收机[M].北京:国防工业出版社,2008.
  • 10Peter Rinder, Nicolaj Bertelsen. Design of a single frequency GPS software receiver. Aalborg University, 2004.

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