Author:
Quan Wei,Gong Xiaolin,Fang Jiancheng,Li Jianli
Publisher
Springer Berlin Heidelberg
Reference52 articles.
1. Baziw J, Leondes CT (1972) In-flight alignment and calibration of inertial measurement units, Part I: General formulation. IEEE Trans Aerosp Electron Syst 8(4):439–449
2. Baziw J, Leondes CT (1972) In-flight alignment and calibration of inertial measurement units, Part II: Experimental results. IEEE Trans Aerosp Electron Syst 8(4):450–465
3. Liu B, Fang Ji (2008) A new adaptive feedback Kalman filter based on observability analysis for SINS/GPS. AcAAS 29(2):430–436
4. Qin Y, Zhang H, Wang S (1998) Theory of Kalman filter and integrated navigation. Northwest industrial university press, Xi’an
5. Geng Y, Cui Z, Zhang H, Fang J (2004) Adaptive fading Kaman filter with applications in integrated navigation system. BUAAJ 30(5):434–437
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