GNSS TECHNOLOGY DETERMINATION OF FLYING MACHINE GUIDANCE PARAMETERS
DOI:
https://doi.org/10.18372/2306-1472.56.5408Keywords:
flying machine, guidance parameters, guidance procedure, landing system, modeling, navigation system, trajectoryAbstract
An algorithm of calculating the guidance parameters for GNSS aircraft landing technology was considered. The simulation and evaluation of calculation parameters error were performed as wellReferences
Agajanov, P.A.; Vorobyyov, V.G.; Kuznetsov, A.A. 1980. Automation of air navigation and air
traffic control. Textbook for Universities of civil aviation. Moscow, Transport. 357 p. (in Russian).
International Standards and Recommended Practices (SARPS). Working Paper ICAO C-WP/11519 13/2/01
Downloads
Published
19-12-2013
How to Cite
Konin, V., Kovalevskiy, E., & Olevinska, T. (2013). GNSS TECHNOLOGY DETERMINATION OF FLYING MACHINE GUIDANCE PARAMETERS. Proceedings of National Aviation University, 56(3), 18–21. https://doi.org/10.18372/2306-1472.56.5408
Issue
Section
AEROSPACE SYSTEMS FOR MONITORING AND CONTROL