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Observability of error states in GPS/INS integration
- Source :
- IEEE Transactions on Vehicular Technology. March, 2005, Vol. 54 Issue 2, p731, 13 p.
- Publication Year :
- 2005
-
Abstract
- Observability properties of errors in an integrated navigation system are studied with a control-theoretic approach in this paper. A navigation system with a low-grade inertial measurement unit and an accurate single-antenna Global Positioning System (GPS) measurement system is considered for observability analysis. Uncertainties in attitude, gyro bias, and GPS antenna lever arm were shown to determine unobservable errors in the position, velocity, and accelerometer bias. It was proved that all the errors can be made observable by maneuvering. Acceleration changes improve the estimates of attitude and gyro bias. Changes in angular velocity enhance the lever arm estimate. However, both the motions of translation and constant angular velocity have no influence on the estimation of the lever arm. A covariance simulation with an extended Kalman filter was performed to confirm the observability analysis. Index Terms--Global Positioning System, GPS/INS, inertial measurement unit (IMU), inertial navigation, lever arm, observability.
Details
- Language :
- English
- ISSN :
- 00189545
- Volume :
- 54
- Issue :
- 2
- Database :
- Gale General OneFile
- Journal :
- IEEE Transactions on Vehicular Technology
- Publication Type :
- Academic Journal
- Accession number :
- edsgcl.131280434