Hybrid IRBM-BPNN Approach for Error Parameter Estimation of SINS on Aircraft

Hybrid IRBM-BPNN Approach for Error Parameter Estimation of SINS on Aircraft

To realize the error parameter estimation of strap-down inertial navigation system (SINS) and improve the navigation accuracy for aircraft, a hybrid improved restricted Boltzmann machine BP neural network (IRBM-BPNN) approach, which combines restricted Boltzmann machine (RBM) and BP neural network (...

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Bibliographic Details
Main Authors: Weilin Guo, Yong Xian, Daqiao Zhang, Bing Li, Leliang Ren
Format: Article
Language:English
Published: MDPI AG 2019-08-01
Series:Sensors
Subjects:
integrated navigation
information fusion
error parameter estimation
hybrid approach
restricted Boltzmann machine
BP neural network
pulse signal
Online Access:https://www.mdpi.com/1424-8220/19/17/3682

Internet

https://www.mdpi.com/1424-8220/19/17/3682

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