Developing a low-cost MEMS IMU/ DGPS integrated system for robust machine automation

20th International Technical Meeting of the Satellite Division of The Institute of Navigation 2007 ION GNSS 2007

Volumn 5, Issue , 2007, Pages 1618-1624

  Geng, Yanrui ^a   Cole, Anthony ^a   Dempster, Andrew ^a   Rizos, Chris ^a,b   Wang, Jinling ^a  

^a UNIVERSITY OF NEW SOUTH WALES   (Australia)

^b IAG

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMATION; ERRORS; GLOBAL POSITIONING SYSTEM; INERTIAL NAVIGATION SYSTEMS; INTEGRATED CONTROL; SOFTWARE TESTING;

ATTITUDE ERROR; AUTOMATION APPLICATIONS; DIFFERENTIAL GPS; EARTH ROTATION; INERTIAL MEASUREMENTS UNITS; INERTIAL SENSOR; INTEGRATED SYSTEMS; LOW GRADE; LOW-COSTS; MACHINE AUTOMATIONS;

KALMAN FILTERS;

EID: 58449135091     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

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2. Yanling Du, Jianye Liu, etc. The Attitude integrated algorithm in complete integrated GPS/SINS navigation system. Chinese space science and technology, 26 (1), 2006
3. J.H. Kim, S.Sukkarieh, etc. On the effects of using heading information during in-flight alignment of a low-cost IMU/GPS integrated system
4. th International technical meeting of the satellite division, 2006, Fort Worth, TX
5. Richard P. Kornfeld, R. John Hansman, and John J. Deyst Single-Antenna GPS based aircraft attitude determination. Journal of the institude of navigation, 45(1), 1998
6. S. Fagin. Recursive Linear Regression Theory, Fading Optimal Filter Theory, and Error Analysis of Optimal Systems. 1964 IEEE Int. Convention
7. th International technical meeting of the satellite division, 2006, Fort Worth, TX
8. Yanrui Geng, Zhongxing Cui, etc. Adaptive fading Kalman filter with applications in integrated navigation system. Journal of Beijing University of Aeronautics and Astronautics, 30(5), 2004