Research Article
A Fault-Tolerant Multiple Sensor Fusion Approach Applied to UAV Attitude Estimation
Table 2
Statistics of UIF-based fault tolerant attitude estimation.
| | Operating condition | | | | |
| | Nominal w/o FDIA | 1.598 | 1.697 | 1.417 | 1.679 | | Nominal w/FDIA | 1.585 | 1.708 | 1.360 | 1.610 | | GPS failure w/FDIA | 3.566 | 5.546 | 2.205 | 3.185 | | Gyro failure w/FDIA | 1.814 | 2.211 | 1.622 | 1.821 | | Mag. failure w/FDIA | 1.890 | 2.111 | 1.534 | 1.892 |
|
|
