Research Article
INS Assisted Fuzzy Tracking Loop for GPS-Guided Missiles and Vehicular Applications
Table 5
HG1700 IMU system specifications.
| | Description | | Units |
| | Output data rate | 100/600 | Hz | | Gyro input range | ±1,000 | deg/sec | | Gyro rate scale factor | 150 | ppm | | Gyro bias (one sigma) | 1 | deg/hr | | Gyro angular random walk | 0.125 | deg/√hr | | Accel. range | ±50 | g | | Accel. linearity | 500 | ppm | | Accel. scale factor | 300 | ppm | | Accel. bias | 1.0 | mg |
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