Integrity Algorithm to Protect against Sensor Faults in Tightly-coupled KF State Prediction

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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

DOI
10.33012/2019.16867
URI
http://hdl.handle.net/10203/279940
Appears in Collection
AE-Conference Papers(학술회의논문)
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