Integrity Algorithm to Protect against Sensor Faults in Tightly-coupled KF State Prediction
Real-time PLKF= Predictive PLKF= max(PLKF,nom, PLKF,meas, Real-time PLKF,state) max(PLKF,nom, PLKF,meas, Predictive PLKF,state) Integrity algorithm against all sensor fault hypotheses can be applied for multi-sensor navigation system both prior to operation and in real-time operation.
- Publisher
- Institute of Navigation
- Issue Date
- 2019-09
- Language
- English
- Citation
32nd International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GNSS+ 2019), pp.594 - 627
- Appears in Collection
- AE-Conference Papers(학술회의논문)
- Files in This Item
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