UNMANNED AERIAL VEHICLE INTEGRATED NAVIGATION COMPLEX

Authors

  • F. M. Zakharin State Research Institute of Aviation, Kyiv
  • S. А. Ponomarenko State Research Institute of Aviation, Kyiv

DOI:

https://doi.org/10.18372/1990-5548.53.12146

Keywords:

Integrated navigation complex, adaptive tuning unmanned aerial vehicle, notation coordinates, accelerometer, angular velocity sensors, course-air sensors, GPS-corrector, noninvariant compensation scheme, procedure of discrete filter.

Abstract

The proposed scheme of construction of an integrated navigation complex of an unmanned aerial vehicle, the basis of which are two subsystems – inertial and course-air. For each subsystem, implementation of algorithms for the complex processing of navigation information from the corresponding navigation sensors and onboard equipment of the Global Positioning System on the basis of a non-invariant compensation circuit is envisaged. The logic of using navigation measurements from both subsystems reflects the adaptation of the navigation complex to the flight conditions of the aircraft. The adaptive navigational complex unmanned aerial vehicle will improve the accuracy of the determination of navigational parameters of the flight, reliability and noise immunity of the aircraft during the flight task.

Author Biographies

F. M. Zakharin, State Research Institute of Aviation, Kyiv

Candidate of Engineering. Senior Researcher

S. А. Ponomarenko, State Research Institute of Aviation, Kyiv

Candidate of Engineering. Senior Researcher

References

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How to Cite

Zakharin, F. M., & Ponomarenko S. А. (2017). UNMANNED AERIAL VEHICLE INTEGRATED NAVIGATION COMPLEX. Electronics and Control Systems, 3(53), 75–83. https://doi.org/10.18372/1990-5548.53.12146

Issue

Vol. 3 No. 53 (2017)

Section

COMPUTER-AIDED DESIGN SYSTEMS

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