Abstract
In this paper, the output data of MEMS gyroscope ADRX150 under different input angular velocity within the temperature range of -30°C~50°C is collected and analyzed. Taking the nonlinear and random characteristics of the output data of MEMS gyroscope ADRX150 into account, the dynamic output data model based on RBF neural network is established, which is training and taking the performance testing with the experimental data collection. The results indicate that, the model has high accuracy and good generalization ability.
Publisher
Trans Tech Publications, Ltd.
Reference7 articles.
1. Hanse, J.G., Honeywell MEMS Inertial Technology & Product Status, Position Location and Navigation Symposium, 2004, p.43 – 48.
2. Jacques Leclerc, MEMs for Aerospace Navigation, Aerospace and Electronic Systems Magazine, IEEE, the 14th Saint Petersburg International Conference on Integrated Navigation Systems, Saint Petersburg, Russia, 2007, 2007, 22(10): 31-36.
3. R. Zhu, D. Sun, Z.Y. Zhou, D.Q. Wang: Measurement. Vol. 40(2007), p.322.
4. N. E. Sheimy, H. Y. Hou, X.J. Niu: IEEE Transactions on instrumentation and measurement. Vol. 57(2008), p.140.
5. J.L. Li, J.C. Fang, W. Sheng: Journal of Beijing University of Aeronautics andAstronautics. Vol. 33(2007), p.1064(In Chinese).
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献