Research Article
Integrated Navigation Fusion Strategy of INS/UWB for Indoor Carrier Attitude Angle and Position Synchronous Tracking
Table 1
Drift simulation conditions of inertial drift of the inertial navigation system.
| | Types of errors | Case 1 | Case 2 | Case 3 |
| | -axis accelerometer drift (ug) | 0 | 10 | 50 | | -axis accelerometer drift (ug) | 0 | 10 | 50 | | -axis accelerometer drift (ug) | 0 | 10 | 50 | | -axis gyroscope drift (deg/h) | 0 | 0.01 | 0.05 | | -axis gyroscope drift (deg/h) | 0 | 0.01 | 0.05 | | -axis gyroscope drift (deg/h) | 0 | 0.01 | 0.05 | | White noise coefficient of deviation | 0 | 0.01 | 0.05 |
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