International Journal of Aeronautical and Space Sciences
- Volume 2 Issue 1
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- Pages.67-77
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- 2001
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- 2093-274X(pISSN)
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- 2093-2480(eISSN)
Performance Testing of Integrated Strapdwon INS and GPS
- Lee, Sang-Joog (Aircraft Division Korea Aerospace Research Institute) ;
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Yoo, Chang-Sun
(Aircraft Division Korea Aerospace Research Institute) ;
- Shim, Yo-Han (Aircraft Division Korea Aerospace Research Institute) ;
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Kim, Jong-Chul
(Aircraft Division Korea Aerospace Research Institute)
- Published : 2001.05.01
Abstract
In recent navigation system, the profitable solution is to integrate the GPS and Stapdwon INS (SDINS) system and its integration allows compensation for shortcomings of each system. This paper describes the hardware preparation and presents the test results obtained from the automobile test of the developed system. The automobile tests was conducted with two kinds of inertial sensors and GPS receivers : short range and middle range test, to verify and evaluate the performance of the integrated navigation system. The reference of position is given by the Differential GPS(DGPS) which has cm-level accuracy to compare the accuracy of system. Kalman filtering is used for integrating GPS and SDINS and this filter effectively allows the long-term stability of GPS to correct and decrease the time deviation error of SDINS.