Abstract
In order to improve the anti-jamming ability and precision of MEMS gyroscope, the physical causes of error were analyzed. The dynamic error mathematical model was constructed using the dynamic theory and analytic method. The dynamic error of micro strap-down inertial navigation system was obtained through the test of calibration and compensation. The feasibility of project which the system used to anti-tank missile was verified through system simulation method.
| Original language | English |
|---|---|
| Pages (from-to) | 567-569 |
| Number of pages | 3 |
| Journal | Xitong Fangzhen Xuebao / Journal of System Simulation |
| Volume | 20 |
| Issue number | 3 |
| State | Published - 5 Feb 2008 |
Keywords
- Dynamic error
- Dynamic theory
- Micro Electromechanical System (MEMS) gyroscope
- Modeling
- Simulation
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