METHOD OF AIRCRAFT LANDING BY CURVILINEAR GLIDE PATHS WITHIN THE BOUNDARY TRAJECTORIES
Journal Title: Вісник Національного Авіаційного Університету - Year 2017, Vol 73, Issue 4
Abstract
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.
Authors and Affiliations
Svitlana Pavlova, Dmytro Voloshenyuk
Keywords
Related Articles
- EP ID EP459645
- DOI 10.18372/2306-1472.73.12169
- Views 144
- Downloads 0
METHOD OF PATH CONSTRUCTING OF INFORMATION ROBOT ON THE BASIS OF UNMANNED AERIAL VEHICLE
Purpose: The purpose of this article is to present a method for constructing the branching path of the information robot (IR) that is a compound dynamic system (CDS) allowing us to formulate, in terms of optimal control...
COMPLIANCE OF DOMESTIC CRIMINAL LAW WITH INTERNATIONAL STANDARDS REGARDING LIABILITY FOR HIJACKING AND SEIZING AN AIRCRAFT
Purpose: the main task of this scientific research is to study the problem of public danger, which arises as a result of the capture or hijacking of an aircraft. The problems of criminal responsibility for this socially...
A HYBRID APPROACH TO THE OPTIMAL AERONAUTICAL ENGINEERING MAINTENANCE PERIODICITY DETERMINATION
Purpose: The goal of this research is to investigate the possibility of the objectively existing aeronautical engineering maintenance optimal periodicity determination in the different from the entirely probabilistic met...
DETERMINATION OF THE INDEX OF CLEARNESS FOR THE DISTRIBUTION OF FUZZY MEASURES
Objective: To justify the need and propose a new clarity i ndex for the distribution of a fuzzy measure with an arbitrary modality. Conduct a study of the new index and show its effectiveness, sensitivity and ease of...
ACOUSTIC RADIATION ENERGY AT A VARIATION OF THE COMPOSITE MECHANICAL DESTRUCTION AREA
Purpose: The technological parameters of composite materials machining and also cutting tool state determine deforming and destruction of their surface layers conditions. Change of this conditi...