Research Article
Reliable SINS/SAR/GNSS Integrated Navigation System for the Supersonic Vehicle
| Parameters | Unit | Value |
| Accelerometer bias | | 100 | Accelerometer scale factor | ppm | 100 | Accelerometer installation | arcsec | 20 | Accelerometer white noise | | 30 | Gyroscope bias | | 0.1 | Gyroscope scale factor | ppm | 100 | Gyroscope installation | arcsec | 20 | Gyroscope white noise | | 0.03 | Update cycle | ms | 0.002 | Mechanization cycle | ms | 0.004 |
|
|