In-flight calibration approach based on quaternion optimization for pos used in airborne remote sensing

IEEE Transactions on Instrumentation and Measurement

Volumn 62, Issue 11, 2013, Pages 2882-2889

  Taizhong, Kang ^a   Jiancheng, Fang ^a   Wei, Wang ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Airborne remote sensing; error promulgation; gyroscope bias error; in flight calibration; position and orientation system; quaternion constrained least square

Indexed keywords

AIRBORNE REMOTE SENSING; ERROR PROMULGATIONS; GYROSCOPE BIAS ERRORS; IN-FLIGHT CALIBRATION; POSITION AND ORIENTATION SYSTEMS; QUATERNION-CONSTRAINED LEAST SQUARES;

ALGORITHMS; FLIGHT SIMULATORS; GYROSCOPES; MOTION COMPENSATION; OPTIMIZATION; REMOTE SENSING;

CALIBRATION;

EID: 84885955336     PISSN: 00189456     EISSN: None     Source Type: Journal    
DOI: 10.1109/TIM.2013.2258243     Document Type: Article

References (25)

1. M. R. Mohamed Mostafa and J. Hutton. (2001). "Direct positioning and orientation systems how do they work? What is the attainable accuracy?" in Proc. Am. Soc. Photogrammetry Remote Sensing Annu. Meeting, pp. 1-11 [Online]. Available: http://www.applanix.com/media/downloads/articles papers/POSAV 2001 04 DirectPositioning.pdf
2. K. Taizhong, F. Jiancheng, and L. Jianli, "Quaternion optimization based in-flight alignment approach for airborne POS," IEEE Trans. Instrum. Meas., vol. 61, no. 11, pp. 2916-2923, Nov. 2012.
3. M. Wu, Y. Wu, X. Hu, and D. Hu, "Optimization-based alignment for inertial navigation systems: Theory and algorithm," Aerosp. Sci. Technol., vol. 15, no. 1, pp. 1-17, May 2010.
4. G. Wahba, "A least squares estimate of spacecraft attitude," SIAM Rev., vol. 7, no. 3, p. 409, Jul. 1965.
5. R. W. Weinman and J. V. Rutkoskie, "Development, performance assessment, and verification of a calibration and alignment technique for a precision IMU," in Proc. Guidance Control Conf., Albuquerque, NM, 19-21 August 1981, pp. 6-15.
6. A. D. Jackson, "Continuous calibration and alignment techniques for an all-attitude inertial platform," in Proc. AIAA Guidance Control Conf., Key Biscayne, FL, USA, Aug. 20-22, 1973, pp. 73-865
7. R. M. Rogers, Applied Mathematics in Integrated Navigation Systems (AIAA Education Series). Reston, VA, USA: American Institute of Aeronautics and Astronautics, 2003.
8. W. Xinlong, "Fast alignment and calibration algorithms for inertial navigation system," Aerosp. Sci. Technol., vol. 13, no. 4-5, pp. 204-209, June-July 2009.
9. W. Xinlong and G. Longhua, "An intelligentized and fast calibration method of SINS on moving base for planed Missiles," Aerosp. Sci. Technol., vol. 13, no. 4-5, pp. 216-223, June-July 2009.
10. M. S. Grewal, "Application of Kalman filtering to the calibration and alignment of inertial navigation systems," in Proc. 29th Conf. Decision Control, Honolulu, HI, USA, Dec. 1991, pp. 3-13.
11. F. Jiancheng and Y. Sheng, "Study on innovation adaptive EKF for inflight alignment of airborne POS," IEEE Trans. Instrum. Meas., vol. 60, no. 4, pp. 1378-1388, Apr. 2011.
12. A. Jamshaid and J. C. Fang, "Alignment of strapdown inertial navigation system: A literature survey spanned over the last 14 years," 2006. Available: http//www.rin.org.uk/site/upload/document/Strapdown INS.pdf.
13. F. Jiancheng and G. Xiaolin, "Predictive iterated Kalman filter for INS/GPS integration and its application to SAR motion compensation," IEEE Trans. Instrum. Meas., vol. 59, no. 4, pp. 909-915, Apr. 2010.
14. T. Beravs, J. Podobnik, and M. Munih, "Three-axial accelerometer calibration using Kalman filter covariance matrix for online estimation of optimal sensor orientation," IEEE Trans. Instrum. Meas., vol. 61, no. 9, pp. 2501-2511, Sep. 2012.
15. Z.-Q. Zhang, X.-L. Meng, and J.-K. Wu, "Quaternion-based Kalman filter with vector selection for accurate orientation tracking," IEEE Trans. Instrum. Meas., vol. 61, no. 10, pp. 2817-2824, Oct. 2012.
16. G. Xiaolin and F. Jiancheng, "Analyses and comparisons of some nonlinear Kalman filters in POS for airborne SAR motion compensation," in Proc. 2007 IEEE Int. Conf. Mechatronics Autom., Harbin, China, pp. 1495-1500.
17. S. P. Dmitriyev and O. A. Stepanov, "Nonlinear filtering methods application in INS alignment," IEEE Trans. Aerosp. Electron. Syst., vol. 33, no.1, pp. 260-271, 1997.
18. H. S. Hong, C. G. Park, and J. G. Lee, "A leveling algorithm for an underwater vehicle using extended Kalman filter," Proc. IEEE Position Location Navigation Symp., CA, USA, 1998, pp. 280-285.
19. K. J. Kim and C. G. Park, "in-flight alignment algorithm based on non-symmetric unscented transformation," SICE-ICASE Int. Joint Conf., 2006, pp. 4916-4920. (Pubitemid 46949871)
20. J. Yang, H. Y. Zhang, and J. Li, "INS nonlinear alignment with large azimuth misalignment angle using predictive filter," J. Chin. Inertial Technol., vol. 1, no. 6, pp. 44-52, 2003.
21. S. J. Julier, and J. K. Uhlmann, "Unscented filtering and nonlinear estimation," Proc. IEEE, vol. 92, no. 3, pp. 401-422, Mar. 2004. (Pubitemid 40890750)
22. T. M. Pham, "Kalman filter mechanization for INS airstart," IEEE Aerosp. Electron. Syst. Mag. (ISSN 0885-8985), vol. 7, no. 1, pp. 3-11, Jan. 1992.
23. I. Y. Bar-Itzhack, "Minimal order time sharing filters for INS in-?ight alignment," J. Guidance, Control, Dyn., vol. 5, no. 4, pp. 396-402, 1982.
24. Y. Tang, Y. Wu, and M. Wu, "INS/GPS integration: Global observability analysis," IEEE Trans. Veh. Technol., vol. 58, no. 3, pp. 1129-1142, Mar. 2009.
25. I. Rhee, M. F. Abdel-Hafez, and J. L. Speyer, "Observability of an integrated GPS/INS during maneuvers," IEEE Trans. Aerosp. Electron. Syst. vol. 40, no. 2, pp. 526-535, Apr. 2004.