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  1541      Downloads  69
Abstract
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.
Keywords
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
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.
Reference
[1]
Oleg S.Salychev, “Inertial Systems in Navigation and Geophysics,” Bauman Moscow State Technical University, Russia, Moscow, 1998.
[2]
C. Krebs, “Generic IMU-camera calibration algorithm: Influence of IMU-axis on each other,” ETH Zrich, Tech. Rep., December 2012.
[3]
Weiguang, G., et al., “Application of adaptive Kalman filtering algorithm in IMU/GPS integrated navigation system”.Geo-spatial Information Science, 2007.
[4]
Nguyen Quang Vinh ."Statistic analysis of the self guidance precision with nonlinearities in the control circle" . //Automatization and modern technology, Moscow, 2006, Number 3, p.11-15 .
[5]
"Process and research on the method of guidance a maneuvering target with scholastic prediction about its motion and with nonlinearities in the control circle" (A report on the scientific researching work)/MSTU named after Bauman.The supervisor: Pupkov K. A. The executors: Nguyen Quang Vinh, Bobkov A.V., Ustiuzanin A.D. /Moscow, 2006, 75 pages.
[6]
Nguyen Duc Anh, Phan Tuong Lai, Nguyen Quang Vinh, (2015) “algorithm detection of fires in forests from the camera in the firefighting aircraft” Journal of Scientific Research and military technology, (6), Pp 12-35.
[7]
Nguyen Quang Vinh, …. A filter for onertia measure system IMU AHRS, Journal of Scientific Research and military technology, (21/2012), tr 7-14.
[8]
Nguyen Quang Vinh, Tran Duc Thuan,… Design, fabrication inertial navigation module with adjustment based sensors integrated microelectromechanical. Journal of Scientific Research and military technology 4/ 2014. Pp. 86-92.
[9]
Nguyen Quang Vinh, Truong Duy Trung,… Guidance, navigation and control of Autonomous underwater vehicle, International Symposium on Electrical-Electronics Engineering Viet Nam (ISEE2013) pp 44-49.
[10]
Nguyen Quang Vinh, INS/GPS integration system using street return algorithm and compass sensor, XII internation symposium Intelligent systems 2016, Moscow, Russia, 2016, p.475-483.
Browse journals by subject