Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《Journal of Civil Aviation Flight University of China》 2012-03
Add to Favorite Get Latest Update

Error Analysis on Integrated SINS/GPS Navigation System Based on Kalman Filter Technique

Wei Lin Xie Guo (Aviation Engineering Institute,Civil Aviation Flight University of China,Guanghan 618307,Sichuan,China)  
Integrated SINS/GPS navigation system error models are analyzed in this paper and a two demotions error analysis method is proposed based on Kalman filter technique in the condition of small misalignment azimuth angle.The GPS/SINS speed and position integrated navigation model of loose coupling combinations under system error equations is established.In different observed quantity combination cases the simulated experiments are carried out,and different observed quantity of system error influence are also discussed.
【Fund】: 中国民航局科研基金(MHRD201022)
【CateGory Index】: V249.328
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
China Proceedings of conference Full-text Database 10 Hits
1 Yang Xiaoxia,Huang Yi Key Laboratory of Systems and Control,CAS,Beijing 100190,P.R.China;Observability Analysis for the Error States of SINS under the Outer Field Conditions[A];[C];2008
2 Du Junwei 1,Sui Shulin 2,Yao wenlong 2 1.College of Information Science and Technology,Qingdao University of Science & Technology,Qingdao 266042,P.R.China 2.Institute of Autonomous Navigation and Intelligent Control,Qingdao University of Science and Technology,Qingdao 266042,P.R.China;The Improved Algorithm of UPF in Spacecraft Autonomous Optical Navigation[A];[C];2008
3 Zhang Yachong Flight Automatic Control Research Institute,Xi’an,710065,P.R.China;On Fault-Tolerant Navigation Technique and Its Application in INS/GPS/Doppler Integrated Navigation System[A];[C];2008
4 MU Yu-Tao,FANG Hai-Tao Key Laboratory of Systems and Control,Academy of Mathematics and Systems Science, Chinese Academy of Sciences,Beijing 100190,P.R.China;One Alignment Method for SINS in Vehicular Environment[A];[C];2011
5 WANG Shengjie~(1,2),KANG Fengju~(1,2),HAN Hong~(1,2) (1.Marine College of Northwestern Polytechnical University,Xi'an,710072,China 2.National Key Laboratory of Underwater Information Process and Control,Xi'an,710072,China);Research on hardware-in-loop simulation system for integrated navigation system of AUV[A];[C];2011
6 GUO Jianjun~1,XIE Pan~2,LIU Juan~2,CUI Haiying~2 (1.Xi'an Ai Sheng Technology Group Engine Division,Xi'an,710072,China; 2.National key Lab,Xi'an,710072,China;);Research on combined navigation of long-range AUV based on federated filter[A];[C];2011
7 PENG Dongli,MA Haitao,XU Weijie (Shanghai Acoustic Laboratory,Institute of Acoustics,Chinese Academy of Sciences,Shanghai 200032,China);The development and application of DVL in integrated navigation technology[A];[C];2011
8 WANG Haihong,ZHENG Jinjun,HE Shanbao,CHU Haibin,HAN Zhigang,LI Changjiang China Academy of Space Technology,Beijing 100094,China;A distributed autonomous orbit determination System based on ground long-term injecting ephemeris parameters of navigation constellation[A];[C];2011
9 Song Huijie,Qu Lili National Time Service Centre,Chinese Academy of Sciences,Xi′an 710600,China;The application of adaptive Kalman filter in clock difference data processing[A];[C];2012
10 ZHANG Jin-liang,QIN Yong-yuan,MEI Chun-bo (College of Automation,Northwestern Polytechnical University,Xi'an 710072);Shoe-mounted personal navigation system based on MEMS inertial sensors[A];[C];2011
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved