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- W3014195659 abstract "There are many systems used to find out the location of the object or vehicle. The most widely used location tracking system is GPS that is the global positioning system. To find out the location of the missile, the inertial navigation system (INS) is used. Inertial measurement unit (IMU) performs the main role in this system, which consists of microelectromechanical system (MEMS) sensors. Accelerometer and gyroscope are used to give linear acceleration and angular rotation. Integrate the rates obtain from accelerometer and gyroscope twice to get velocity and position. To obtain the exact position of the missile, it is necessary to reduce the Coriolis effect from the rates. This survey paper elaborates on the modeling and simulation of the INS (Brown in Test results of a GPS/inertial navigation system using a low cost MEMS IMU, 04 2004 [1])." @default.
- W3014195659 created "2020-04-10" @default.
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- W3014195659 date "2020-01-01" @default.
- W3014195659 modified "2023-10-18" @default.
- W3014195659 title "Modeling and Simulation of Inertial Navigation System" @default.
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- W3014195659 doi "https://doi.org/10.1007/978-981-15-2329-8_48" @default.
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