Synthesis of StrapdownInertial Navigation SystemUsing Feedback-Feedforward Correction with GPS and Altimeter as References
Theobjective of this research is to design a prototype of strapdown inertial navigation system (SINS) for RKX-200 rocket made by LAPAN. The SINS is designed by integration of inertial measurement unit (IMU) and GPS (Global Positioning System) with an altimeter as the references using Kalman Filte...
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| Format: | Final Project |
| Language: | Indonesia |
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| Online Access: | https://digilib.itb.ac.id/gdl/view/44889 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |