OPTIMAL CHOICE OF HARDWARE COMPLEXES OF VISUAL NAVIGATION SYSTEM UAV

Authors

  • V. M. Sineglazov National Aviation University
  • V. S. Ischenko National Aviation University

DOI:

https://doi.org/10.18372/1990-5548.47.10289

Keywords:

Visual navigation system, unmanned aerial vehicle, camera, flight controller

Abstract

The design problem of unmanned aerial vehicle visual navigation system is considered. It isproposed the method of technical means selection of visual navigation system based on the use ofhierarchies analysis method

Author Biographies

V. M. Sineglazov, National Aviation University

Doctor of Engineering. Professor. Aviation Computer-Integrated Complexes Department

V. S. Ischenko, National Aviation University

Graduade student. Aviation Computer-Integrated Complexes Department

References

V. A. Rogoshyn, V. M. Sineglazov and N. K. Filyashkin, Flight Navigation Complexes of Aircrafts. Kyiv, NAU, 2004, 238 p. (in Ukrainian).

Flight controller Pixhawk http://pixhawk.org

Paul D. Groves, Principles of GNSS, Inertial, and Multisensor Integrated Navigation Systems. Second Edition (Artech House Remote Sensing Library) 2nd Edition, 2008, 503 p.

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How to Cite

Sineglazov, V. M., & Ischenko, V. S. (2016). OPTIMAL CHOICE OF HARDWARE COMPLEXES OF VISUAL NAVIGATION SYSTEM UAV. Electronics and Control Systems, 1(47), 80–87. https://doi.org/10.18372/1990-5548.47.10289

Issue

Vol. 1 No. 47 (2016)

Section

COMPUTER-AIDED DESIGN SYSTEMS

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