Volume 5, Issue 2, April 2017, Page: 78-84
Combination of an Inertial Measurement Unit and a Camera for Defining the Position of an Airplane
Nguyen Quang Vinh, Department of Radio-Electronic, Institute of Science and Technology, Hoang sam, Cau Giay, Ha Noi, Viet Nam
Received: Sep. 21, 2016;       Accepted: Feb. 10, 2017;       Published: Mar. 15, 2017
DOI: 10.11648/j.sjams.20170502.13      View  1824      Downloads  107
In this article we propose a method of using the extended Kalman filter combined with an inertial navigation system and a camera to assist in determining the location and calculate the parameters of a helicopter. These observations are combined with an inertial measurement instrument which uses the Kalman filter to collect accurately and promptly information about the location of a plane. The algorithms is simulated on Simulink and hardened by using dsPIC33F256 chip.
Inertial Navigation Systems, Kalman, Helicopter
To cite this article
Nguyen Quang Vinh, Combination of an Inertial Measurement Unit and a Camera for Defining the Position of an Airplane, Science Journal of Applied Mathematics and Statistics. Vol. 5, No. 2, 2017, pp. 78-84. doi: 10.11648/j.sjams.20170502.13
Copyright © 2017 Authors retain the copyright of this article.
This article is an open access article distributed under the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0/) which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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