METHOD OF AIRCRAFT LANDING BY CURVILINEAR GLIDE PATHS WITHIN THE BOUNDARY TRAJECTORIES
DOI:
https://doi.org/10.18372/2306-1472.73.12169Keywords:
aircraft, air traffic, border trajectory, curvilinear glide path, landing methodAbstract
Purpose: The paper is dedicated to improving of civil aviation flight safety question by the way of new method of aircraft landing by curvilinear glide paths within the boundary trajectories. Proposed method ordered for improving of safety level, sustainability and cost effectiveness of the aircraft landing with own individual, optimal vertical descending profile from flight level to the runway threshold. Methods: Landing method, based on generation (calculation and construction) of virtual curvilinear glide paths of landing within the boundary trajectories with taking into account of “fully controllable state areas” of aircraft has been proposed. Results: New aircraft landing method that has large profit in the reducing of the level of noises, fuel consumption and harmful emissions. Discussion: The essence of the method consists in using of fully controllable state areas that are constructed taking into account on linearity in aircraft flight characteristics, probable changes into environmental state, criterion of landing implementation optimality, all functional and aerodynamic aircraft capabilities for virtual curvilinear glide path construction, meant by some aircraft traffic trajectory for time and distance reducing, that are necessary for stage from start of descending from flight level to runway threshold.
References
Pavlov V.V., Skripets A.V. (2000), Ergonomicheskie voprosy sozdaniya i ekspluatatsii aviatsionnyih elektrifitsirovannyih i pilotazhno-navigatsionnyih kompleksov vozdushnyih sudov [Ergonomic questions of electrified aeronautic and flight control complex creation and exploitation]. Kyiv, “KMUGA” Publ., 460 p. (In Russian)
Rogozhyin V.O., Sineglazov V.M., Filyaschkin M.K. (2005), Pilotazhno-navigatsiyni kompleksy povitryanyh sudden: Pidruchnyik [Flight control complexes of airborne vehicles: Handbook] – Кyiv: “NAU” Publ., – 502 p. (In Ukrainian)
The ICAO circulars on ergonomics and human factors (№. 1-12) (2000), – “ІСАО”.
Teryaev E.D., Petrin K.V. (2009), Development of the concept of flexible trajectories in the backs of the terminal control moving objects. Bulletin of the Institute of Mechanical Engineering RAS – Мoscow. – pp. 18-23.
Petrov B.N., Portnov-Sokolov Yu.P., Andrienko A.Ya., Ivanov V.P. (1983), Onboard terminal management system: Principles and elements of the theory – Мoscow: “Mashinostroenie” Publ., – 542 p.
Bek V.V., Vishnyakov Yu.S., Mahlin A.R. (1989) Integrated systems of the terminal control – Мoscow: “Nauka” Publ., – 254 p.
A.A. Zhevnin, K.S. Kolesnikov (1985), Synthesis of terminal control algorithms based on the concept of inverse problems of dynamics. Bulletin of the Academy of Sciences of the USSR. “Tehn. Cybernetics”, issue no. 4, – pp. 180-188.
Mhitaryan A.M., Laznyuk P.S., Maksimov V.S. and other (1978) Aircraft Flight Dynamics. – Мoscow, “Mashinostroenie”, 424 p.
Continuous descent approach. Wikipedia the free encyclopedia – available at: https://en.wikipedia.org/wiki/ Continuous _descent_ approach.
International civil Aviation Vocabulary Doc 9713 (2007), - issue no. 3., Montreal, ІСАО. – 816p.
Continuous Descent Operation (CDO) Doc ICAO 9331 – “Erwin Lassooij PBN program office, ICAO/International civil aviation organization” Publ., – available at: http://www.icao.int/icaonet/.
Pavlova S., Volkov O. (2017), System of guaranteed resolution of dynamic conflicts of aircrafts in real time. Proceedings of the National Aviation University: Scientific journal: scientific article. – Kyiv, . № 1. pp. 29-35.