GPS/INS/Seeker Integrated Navigation System for the Case of GPS Blockage ()
Woo Hyun Kim,
Jang Gyu Lee,
Hyung Keun Lee,
Chan Gook Park
School of Electrical Engineering and Computer Science, Seoul National University, 133-dong, ASRI #610, San 56-1, Sillim-dong, Gwanak-gu, Seoul, 151-742, South Korea.
School of Electronics, Telecommunication & Computer Eng., Korea Aerospace University, 200-1, Hwajon-dong, Deokyang_gu, Goyang-city, Kyunggi-do, 412-791, South Korea.
School of Mechanical and Aerospace Engineering, Seoul National University, San 56-1, Sillim-dong, Gwanak-gu, Seoul, 151-744, South Korea.
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Abstract
When GPS blockage occurs for a loosely coupled GPS/INS system, its navigation error diverges. To deal with such cases, this paper introduces an integration scheme for GPS, INS, and an image sensor. The proposed integration scheme is attractive in that it accomplished the position and velocity accuracy improvement by the angular information only. The angular information is provided by the gimbal angles of the image sensor. A realistic scenario is studied by a simulation to demonstrate that the GPS/INS/Image integrated navigation system works effectively.
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W. Kim, J. Lee, H. Lee and C. Park, "GPS/INS/Seeker Integrated Navigation System for the Case of GPS Blockage," Positioning, Vol. 1 No. 10, 2006, pp. -.
Conflicts of Interest
The authors declare no conflicts of interest.
References
[1]
|
Maybeck P.S. (1994) Stochastic Models, Estimation, and Control, Vol.1, Navtech Book & Software Store pp.291~297.
|
[2]
|
Park Y.B. (2001) Design of Integrated INS/GPS/Odometer Navigation System and Its Performance Analysis, School of Electronical Engineering and Computer Science, Seoul National University.
|
[3]
|
Titterton D.H., Weston J.L. (1997) Strapdown inertial navigation technology, Peter Peregrinus Ltd., pp.363~394.
|
[4]
|
Vathal S. (1987) Spacecraft Attitude Determination Using a Second-Order Nonlinear Filter, Journal of Guidance and Control, Vol.10, No 6, pp.559~565.
|
[5]
|
Young R.M. (2005) Feedback Linearization Control of a 2-Axis Gimbal Seeker in BTT Missile, School of Electronical Engineering and Computer Science, Seoul National University.
|