Browse > Article
http://dx.doi.org/10.12673/jant.2022.26.4.235

An Analysis of the Attitude Estimation Errors Caused by the Deflection of Vertical in the Initial Alignment  

Kim, Hyun-seok (Agency for Defense Development)
Park, Chan-sik (Dept. of Intelligent Systems and Robotics, Research Institute for Computer and Information Communication, Chungbuk Natioinal University)
Abstract
In this paper, in the case of an inertial navigation system, the posture estimation error in the initial alignment due to vertical deflection is analyzed. Posture estimation error due to DOV was theoretically analyzed based on the speed and posture error of INS. Simulations were performed to verify the theoretical grinding, and the results were in good agreement. For example, in the case of η=20", an alignment error of ϕN=0.00287°, ϕU=0.00196° occurred, and in the case of 𝜉=20", an error of ϕE= -0.00286° occurred. Through this, it was confirmed that the vertical posture error caused by the DOV occurred as a coupling characteristic of the INS posture error. It has been shown that an additional posture error may occur due to the DOV, which was not considered in the existing INS alignment, which means that correction for the DOV must be considered when applying high-precision INS.
Keywords
Inertial Navigation system; Initial Alignment; Deflection of Vertical; Attitude Error; Horizontal Gravity Disturbance;
Citations & Related Records
연도 인용수 순위
  • Reference
1 D. Grejner-Brzezinska, C. Toth, Y. Yi, "On improving navigation accuracy of gps/ins systems", Photogrammetric Engineering and Remote Sensing, No. 4, pp. 377-389, Apr. 2005.
2 R. M. Rogers, Applied Mathmatics in Integrated Navigation Systems, 3rd ed. Reston, VA: American institute of Aeronautics and Astronautics, 2007.
3 J. Tie, J. Cao, M. Wu, J. Lian, S. Cai, L. Wang, "Compensation of horizontal gravity disturbances for high precision inertial navigation", MDPI Sensors, Vol. 18, No. 3 : 906, Mar. 2018.
4 D.W. Harriman, C. Van Dam, "Gravity-induced errors in airborne inertial navigation," The Journal of Guidance, Control and Dynamics, Vol. 9, No. 4, pp. 419-426, May. 1986.   DOI
5 N.K. Pavlis, S.A. Holmes, S.C. Kenyon, J.K. Factor, "An earth gravitational model to degree 2160: Egm2008", EGU General Assembly, Vienna, Austria, pp.13-18, 2008.
6 X. Zhou, G. Yang, G. J. Wang, Z. Wen, "A combined gravity compensation method for ins using the simplified gravity model and gravity database", MDPI Sensors, Vol. 18, No. 5 : 1552, May. 2018.
7 D. A. Grejner-Brzezinska, R. Da, R. C. Toth, "Gps error modeling and otf ambiguity resolution for high-accuracy gps/ins integrated system", Journal of Geodesy, Vol. 72, pp. 626-638, 1998.   DOI
8 Dai, D.; Wang, X.; Zhan, D.; Qin, S.; Huang, Z. "Dynamic measurement of high-frequency deflections of the vertical based on the observation of ins/gnss integration attitude error", Journal of Applied Geophysics, Vol. 119, pp. 89-98, May. 2015.   DOI
9 P.D. Groves, Principles of Gnss, Inertial, and Multisensor Integrated Navigation Systems, Norwood, MA, USA, Artech House, 2013.
10 J.A. richeson, "Gravity Gradiometer Aided Inertial Navigation within Non-Gnss Environments, Ph.D. Thesis, University of Maryland, College Park, MD. USA, Jan. 2008.
11 C. Jekeli, "Gravity on precise, short-term, 3-d free-inertial navigation", Navigation: Journal of the Institute of Navigation, Vol. 44, No. 3, pp. 347-358, 1997.   DOI
12 D. Dai, X. Wang, D. Zhan, Z. Huang, "An improved method for dynamic measurement of deflections of the vertical based on the maintenance of attitude reference", MDPI Sensors, Vol. 14, No. 9 : 16322-16342, Sept. 2014.   DOI
13 C. Jekeli, "Precision free-inertial navigation with gravity compensation by an onboard gradiometer," The Journal of Guidance, Control and Dynamics, Vol. 29, No. 3, pp. 704-713, May. 2006.   DOI
14 R. Wu, Q. Wu, F. Han, T. Liu, P. Hu, H. Li, "Gravity compensation using egm2008 for high-precision long-term inertial navigation systems", MDPI Sensors, Vol. 16, No. 12 : 2177, Dec. 2016.
15 B. Hofmann-Wellenhof, H. Moritz, Physical Geodesy, 2nd ed. NewYork, NY: SpringerWienNewYork, 2006.
16 H. Xiong, D. Dai, Y. Zhao, X. Wang, J. Zheng, "An analysis of the effect of gravity anomaly to attitude estimation in high-precision gnss/ins integrated navigation systems under overturning cases", In Proceedings of the 2018 DGON Inertial Sensors and Systems (ISS), Braunschweig, Germany, pp. 1-15, Sept. 2018.