Olevinska T. Satellite system navigation efficiency increasing during aircraft landing

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0418U003425

Thesis Registration Form

0418U003425.pdf

Applicant for

Specialization

  • 05.22.13 - Навігація та управління рухом

16-10-2018

Specialized Academic Board

Д 26.062.03

National Aviation University

Essay

The thesis is devoted to the complex solving of the task of developing the model of small aircraft landing by the Global Navigation Satellite System on the regional aerodrome which is not equipped with radio beacon system for precise landing.The model of calculation of aircraft deviation from the glide slope enables simplifying calculation and decreases the number of runway data block parameters. The improved model of integrity monitoring allows to continue landing in case of absence of redundant pseudorange measures. The third model allows to carry out the aircraft indicated air speed calculation in a case of the Air Data System failure by providing a quantitative determination of the current speed.

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Files

autoreferat--Олевінська_Автореферат.pdf

Дисертація_Олевінська.pdf

Олевінська_Автореферат.pdf

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