Fast in-flight alignment method for MIMU under large attitude errors

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 28, Issue 6, 2007, Pages 1395-1400

  Cao, Juanjuan ^a   Fang, Jiancheng ^a   Sheng, Wei ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

EKF; GPS; In flight alignment; MIMU; Predictive filter; Strapdown inertial navigation system; UKF

Indexed keywords

ALIGNMENT; COMPUTER SIMULATION; GLOBAL POSITIONING SYSTEM; KALMAN FILTERS; MEMS;

IN FLIGHT ALIGNMENT; PREDICTIVE FILTER; STRAPDOWN INERTIAL NAVIGATION SYSTEM;

INERTIAL NAVIGATION SYSTEMS;

EID: 37449017262     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (11)

1. Dmitriycv S P, Stepanov O A. Nonlinear filtering methods application in INS alignment [J]. IEEE Transaction on Aerospace and Electronic Systems, 1997, 33(1): 260-271.
2. Hong H S, Park C G, Lee J G. A leveling algorithm for an underwater vehicle using extended Kalman filter [C]//Proc IEEE Position Location and Navigation Symp. CA, USA: IEEE, 1998: 280-285.
3. Julier S J, Uhlmann J K. Unscented filtering and nonlinear estimation [J]. Proceedings of the IEEE, 2004, 92(3): 401-422.
4. Crassidis J L, Markley F L. Predictive filtering for nonlinear systems [J]. Journal of Guidance, Control and Dynamics, 1997, 20(3): 566-572.
5. Yang Jing, Zhang Hongyue, Li Ji. INS nonlinear alignment with large azimuth misalignment angle using predictive filter [J]. Journal of Chinese Inertial Technology, 2003, 11(6): 44-52. (in Chinese)
6. Zhang Hongmei, Deng Zhenglong, Lin Yurong. UKF method based on model error prediction [J]. Acta Aeronautica et Astronautica Sinica, 2004, 25(6): 598-601. (in Chinese)
7. Hong H S, Lee J G, Park C G. Performance improvement of in-flight alignment for autonomous vehicle under large initial heading error [J]. IEE Proc-Radar Sonar Navig, 2004, 151(1): 57-62.
8. Hong H S, Lee J G, Park C G. In-flight alignment of SDI-NS under large initial heading error [C]//AIAA Guidance, Navigation, and Control Conference and Exhibit. Montreal, Canada: AIAA, 2001: 1-6.
9. Yu M J, Park H W, Jeon C B. Equivalent nonlinear error models of strapdown inertial navigation systems [R]. AIAA-97-3563, 1997: 581-587.
10. Yu M J, Lee J G, Park H W. Comparison of SDINS inflight alignment using equivalent error models [J]. IEEE Transaction on Aerospace and Electronic Systems, 1999, 35(3): 1046-1054.
11. Wei C L, Zhang H Y. SINS in-flight alignment using quaternion error models [J]. Chinese Journal of Aeronautics, 2001, 14(3): 166-170.