相位平滑伪距GNSS PPP/INS紧耦合算法Research of the tight coupling navigation technology of GNSS PPP/INS with phase smoothing pseudo range
燕欢;罗孝文;郭杭;
摘要(Abstract):
针对在导航实践中低成本MEMS使用传统紧耦合方法计算精度受到限制的问题,提出了一种采用载波相位平滑伪距GNSS PPP/INS紧耦合的算法。实验表明,使用相位平滑伪距的GNSS PPP/INS紧耦合方法后低精度的MEMS和GPS组合位置精度为dm级,速度精度为cm/s甚至mm/s,比传统C/A码紧耦合定位精度高,有较好的收敛性;其次当增加相位平滑的历元数后精度也相应提高。当出现GPS信号中断时,该方法能够加速中断以后滤波收敛的速度,将导航精度控制在中高精度惯导作业要求范围内。该方法节约了导航作业的设备成本,具有一定实际意义。
关键词(KeyWords): 组合导航;紧耦合;精密单点定位;相位平滑伪距;卡尔曼滤波
基金项目(Foundation): 国家自然科学基金项目(41374039,41164001)
作者(Authors): 燕欢;罗孝文;郭杭;
DOI: 10.16251/j.cnki.1009-2307.2017.03.005
参考文献(References):
- [1]刘经南,叶世榕.GPS非差相位精密单点定位技术探讨[J].武汉大学学报:信息科学版,2002,27(3):234-240.(LIU Jingnan,YE Shirong.GPS precise point positioning using undifferenced phase observation[J].Geomatics and Information Science of Wuhan University,2002,27(3):234-240.)
- [2]秦永元,汪淑华.卡尔曼滤波与组合导航原理[M].西安:西北工业大学出版社,2010:1.(QIN Yongyuan,WANG Shuhua.Kalman filtering and integrated navigation theory[M].Xi′an:The Northwestern Polytechnical University press,2010:1.)
- [3]杨春燕,吴德伟,卢艳娥,等.基于补充卡尔曼滤波的载波相位平滑伪距算法[J].空军工程大学学报:自然科学版,2008,9(5):52-56.(YANG Chunyan,WU Dewei,LU Yane,et al.A-phase-smoothed pseudorange algorithm based on complementary Kalman filtering[J].Journal of Air Force Engineering University:Natural Science Edition,2008,9(5):52-56.)
- [4]刘海颖,王惠南.基于广义卡尔曼滤波的伪距组合GPS/INS导航[J].航天控制,2004,22(4):52-56.(LIU Haiying,WANG Huinan.The GPS/INS pseudo range integrated navigation based on extend Kalman filtering[J].Aerospace Control,2004,22(4):52-56.)
- [5]孟羹,朱立新.基于GPS/INS紧组合导航的UKF和CKF滤波精度分析[J].航天控制,2014,32(1):10-15.(MENG Yan,ZHU Lixin.Cubature and unscented Kalman filter accuracy analysis based on tightly-coupled GPS/INS integrated navigation system[J].Aerospace Control,2014,32(1):10-15.)
- [6]刘帅,孙付平,李海峰,等.前后向平滑算法在精密单点定位/INS紧组合数据后处理中的应用[J].中国惯性技术学报,2015,23(1):85-91.(LIU Shuai,SUN Fuping,LI Haifeng,et al.Forward-backward-smoothing algorithm with application to tightly coupled PPP/INS data post-processing[J].Journal of Chinese Inertial Technology,2015,23(1):85-91.)
- [7]秦永元.惯性导航原理[M].北京:科学出版社,2005.(QIN Yongyuan.Inertial navigation principle[M].Beijing:Science Press,2005.)
- [8]ROESLER G,MARTELL H.Accuracy tightly coupled processing of precise point position(PPP)and INS data[J].Department of Geomatics Engineering,University of Calgary,2011(1):147-162.
- [9]DU Shuang,GAO Yang.Inertial aided cycle slip detection and identification for integrated PPP GPS and INS[J].Sensors,2012,12(11),344-362.
- [10]RABBOU M A,El-RABBANY A.Tightly coupled integration of GPS precise point positioning and MEMSbased inertial systems[J].GPS Solut,2014:1-9.
- [11]MADEIRA S,YAN Wenlin,BASTOS L,et al.Accuracy assessment of the integration of GNSS and a MEMS IMU in a terrestrial platform[J].Sensors,2014,14(11):866-881.
- [12]FUJITA K,OKUDAIRA T,OKUDAIRA K.Conceptual study and key technology development for Mars aero fly by sample collection[J].Acta Astronautics,2014,93(1):84-93.