Click on the download icon to access/download papers. Papers are immediately available to ION Members on a pay-per access basis. All papers are in PDF format (Adobe Acrobat Reader is required).

Members Only LoginION Members: Sign in for immediate paper access!
Add Paper to CartNon-members: Purchase this paper for $25

Title:An Intelligent Scheme for Rapid INS Alignment Procedure Using Artificial Neural Networks
Author:Yun-Wen Huang, Yu-Sheng Huang and, Kai-Wei Chiang
Meeting: Proceedings of the 2007 National Technical Meeting of The Institute of Navigation
January 22 - 24, 2007
The Catamaran Resort Hotel
San Diego, CA
Page(s):320 - 326
Cite this article:Huang, Yun-Wen, and, Yu-Sheng Huang, Chiang, Kai-Wei, "An Intelligent Scheme for Rapid INS Alignment Procedure Using Artificial Neural Networks," Proceedings of the 2007 National Technical Meeting of The Institute of Navigation, San Diego, CA, January 2007, pp. 320-326.
Abstract:Inertial navigation systems are commonly used in several applications such as aerospace systems and land vehicle navigation. The navigation parameters including position, velocity and attitude of a moving platform are determined by processing the measurement of inertial sensors. In general, the accuracy of the navigation solutions provided by an INS depends on the initial attitude angles of the body frame where the measurements of specific forces and angular rate are sensed by the inertial measurement unit and the navigation frame applied. Therefore, those initial angles have to be estimated accurately prior to switching the INS into navigation mode. The techniques to estimate those initial attitude angles are known as the process of alignment. An optimal estimator, the Kalman filter, takes about 10 to 15 minutes to converge then achieve the alignment process due to measurement errors. Those errors increase the alignment time and deteriorate the overall accuracy of initial attitude angels estimated. Therefore, this article suggested an intelligent alignment scheme that combines an Artificial neural network and Kalman filter to improve the accuracy of initial attitude angles and reduce the consumption of time. In this study, a navigation grade inertial measurement unit was applied to verify the performance of proposed scheme. The preliminary results presented in this article indicate that a faster alignment procedure with higher accuracy can be achieved through the use of proposed scheme.
Is there an error in this record? Help us fix it.