2015Sensor WorldRequires access

Design of a SINS/GPS-integrated navigation system

Guo Yon

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Abstract

Strap-down Inertial Navigation System(SINS) is a kind of navigation way with high degree of autonomy, which is superior to other ways in short-term precision performances, but high in long-term position errors because of accumulative effects. On the other hand, Global Position System(GPS) is good in long-term accuracy, but poor in short-term accuracy. The motivation for GPS/SINS integration is to develop a navigation system which overcomes the shortcomings of each system. This system adopts inertial measurement units(IMUs) to provide linear acceleration and angular velocity, combining with GPS-OEM board to provide GPS information, and high performance DSP to calculate the navigation information. At last, the experiments verify that the system can be applied to practical application

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What this paper is about

Strap-down Inertial Navigation System(SINS) is a kind of navigation way with high degree of autonomy, which is superior to other ways in short-term precision performances, but high in long-term position errors because of accumulative effects. On the other hand, Global Position System(GPS) is good in long-term accuracy, but poor in short-term accuracy. The motivation for GPS/SINS integration is to develop a navigation system which overcomes the shortcomings of each system. This system adopts inertial measurement units(IMUs) to provide linear acceleration and angular velocity, combining with GPS-OEM board to provide GPS information, and high performance DSP to calculate the navigation information. At last, the experiments verify that the system can be applied to practical application

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Available abstract

Strap-down Inertial Navigation System(SINS) is a kind of navigation way with high degree of autonomy, which is superior to other ways in short-term precision performances, but high in long-term position errors because of accumulative effects. On the other hand, Global Position System(GPS) is good in long-term accuracy, but poor in short-term accuracy. The motivation for GPS/SINS integration is to develop a navigation system which overcomes the shortcomings of each system. This system adopts inertial measurement units(IMUs) to provide linear acceleration and angular velocity, combining with GPS-OEM board to provide GPS information, and high performance DSP to calculate the navigation information. At last, the experiments verify that the system can be applied to practical application

Key concepts: Global Positioning System, Inertial navigation system, Navigation system, GPS/INS, Term (time), Computer science, Position (finance), Inertial measurement unit

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