Name
Title | ||
|---|---|---|
A Self-Calibration Method for Accelerometer Nonlinearity Errors in Triaxis Rotational Inertial Navigation System. |
Abstract | ||
|---|---|---|
The navigation performance of the rotational inertial navigation system (RINS) could be greatly improved by rotating the inertial measurement unit with gimbals, and self-calibration for error parameters could be achieved in RINS as well. However, accelerometer nonlinearity errors need to be considered and calibrated to further improve the navigation accuracy of RINS, especially in large dynamic ap... |
Year | DOI | Venue |
|---|---|---|
2017 | 10.1109/TIM.2016.2625958 | IEEE Transactions on Instrumentation and Measurement |
Keywords | Field | DocType |
Accelerometers,Calibration,Mathematical model,Inertial navigation,Estimation,Kalman filters | Inertial navigation system,Observability,Control theory,Accelerometer,Simulation,Control engineering,Kalman filter,Optimal estimation,Inertial measurement unit,Mathematics,Calibration,Gimbal | Journal |
Volume | Issue | ISSN |
66 | 2 | 0018-9456 |
Citations | PageRank | References |
4 | 0.55 | 4 |
Authors | ||
4 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| Pengyu Gao | 1 | 5 | 1.61 |
| Kui Li | 2 | 4 | 1.23 |
| Lei Wang | 3 | 401 | 111.60 |
| Zengjun Liu | 4 | 6 | 2.02 |