SINS/GPS Tightly Integrated Navigation Based on Improved Adaptive Kalman Filter

FANG De-jun

doi:10.3969/j.issn.1671-637x.2017.10.020

Journals >Electronics Optics & Control >Volume 24 >Issue 10 >Page 102 > Article

Electronics Optics & Control
Vol. 24, Issue 10, 102 (2017)

SINS/GPS Tightly Integrated Navigation Based on Improved Adaptive Kalman Filter

FANG De-jun

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[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2017.10.020 Cite this Article

FANG De-jun. SINS/GPS Tightly Integrated Navigation Based on Improved Adaptive Kalman Filter[J]. Electronics Optics & Control, 2017, 24(10): 102 Copy Citation Text

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References

[4] GROVES P D.Principles of GNSS,inertial,and multisensor integrated navigation system［M］.Norwood,MA:Artech House,2008.

[5] HONG S,CHUN H H,KWON S H,et al.Observability measures and their application to GPS/INS［J］.IEEE Transactions on Aerospace and Electronic System,2008, 57(1):97-106.

[10] YANG Y,ZHANG S.Adaptive fitting of systematic errors in navigation［J］.Journal of Geodesy,2005,79(1/2/3):43-49.

FANG De-jun. SINS/GPS Tightly Integrated Navigation Based on Improved Adaptive Kalman Filter[J]. Electronics Optics & Control, 2017, 24(10): 102

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