Name
Title | ||
|---|---|---|
An Accelerometers-Size-Effect Self-Calibration Method for Triaxis Rotational Inertial Navigation System. |
Abstract | ||
|---|---|---|
Rotational inertial navigation system (RINS) could improve navigation performance by rotating the inertial measurement unit (IMU) with gimbals, and error parameters could be self-calibrated as well. However, accelerometers size effect would cause more influence on navigation accuracy in RINS than a strapdown inertial navigation system because of gimbals rotation, which should be calibrated and com... |
Year | DOI | Venue |
|---|---|---|
2018 | 10.1109/TIE.2017.2733491 | IEEE Transactions on Industrial Electronics |
Keywords | Field | DocType |
Accelerometers,Acceleration,Calibration,Angular velocity,Inertial navigation,Observability | Inertial navigation system,Angular velocity,Accelerometer,Control theory,Inertial measurement unit,Acceleration,Engineering,Inertial reference unit,Calibration,Gimbal | Journal |
Volume | Issue | ISSN |
65 | 2 | 0278-0046 |
Citations | PageRank | References |
1 | 0.39 | 6 |
Authors | ||
4 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| Pengyu Gao | 1 | 5 | 1.61 |
| Kui Li | 2 | 1 | 0.39 |
| Tianxiao Song | 3 | 1 | 1.40 |
| Zengjun Liu | 4 | 6 | 2.02 |