1. Hybrid IRBM-BPNN Approach for Error Parameter Estimation of SINS on Aircraft
- Author
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Yong Xian, Leliang Ren, Bing Li, Daqiao Zhang, and Weilin Guo
- Subjects
0209 industrial biotechnology ,Computer science ,pulse signal ,integrated navigation ,02 engineering and technology ,BP neural network ,lcsh:Chemical technology ,Biochemistry ,Parameter error ,Article ,Analytical Chemistry ,020901 industrial engineering & automation ,Inertial measurement unit ,Position (vector) ,0202 electrical engineering, electronic engineering, information engineering ,information fusion ,lcsh:TP1-1185 ,Electrical and Electronic Engineering ,Instrumentation ,Inertial navigation system ,error parameter estimation ,Restricted Boltzmann machine ,Artificial neural network ,business.industry ,Navigation system ,Atomic and Molecular Physics, and Optics ,Global Positioning System ,020201 artificial intelligence & image processing ,business ,Algorithm ,restricted Boltzmann machine ,hybrid approach - Abstract
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 (BPNN), is proposed to forecast the inertial measurement unit (IMU) instrument errors and initial alignment errors of SINS. Firstly, the error generation mechanism of SINS is analyzed, and initial alignment error model and IMU instrument error model are established. Secondly, an unsupervised RBM method is introduced to initialize BPNN to improve the forecast performance of the neural network. The RBM-BPNN model is constructed through the information fusion of SINS/GPS/CNS integrated navigation system by using the sum of position deviation, the sum of velocity deviation and the sum of attitude deviation as the inputs and by using the error parameters of SINS as the outputs. The RBM-BPNN structure is improved to enhance its forecast accuracy, and the pulse signal is increased as the input of the neural network. Finally, we conduct simulation experiments to forecast and compensate the error parameters of the proposed IRBM-BPNN method. Simulation results show that the artificial neural network method is feasible and effective in forecasting SINS error parameters, and the forecast accuracy of SINS error parameters can be effectively improved by combining RBM and BPNN methods and improving the neural network structure. The proposed IRBM-BPNN method has the optimal forecast accuracy of SINS error parameters and navigation accuracy of aircraft compared with the radial basis function neural network method and BPNN method.
- Published
- 2019
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