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Requisitos modernos para equipos de navegación de aeronaves con inmunidad al ruido de Oleg Iva-

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Modern Requirements for Noise Immunity Aircraft Navigation Equipment by Oleg Iva
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Características del artículo

Estado
Nuevo: Libro nuevo, sin usar y sin leer, que está en perfecto estado; incluye todas las páginas sin ...
ISBN-13
9789811600722
Type
NA
Publication Name
NA
ISBN
9789811600722
Book Title
Modern Requirements for Noise Immunity Aircraft Navigation Equipment
Book Series
Springer Aerospace Technology Ser.
Publisher
Springer
Item Length
9.3 in
Publication Year
2021
Format
Hardcover
Language
English
Illustrator
Yes
Author
Oleg Ivanovich Zavalishin, Yury Grigoryevich Shatrakov, Dmitry Alexandrovich Zatuchny
Genre
Technology & Engineering, Science
Topic
Aeronautics & Astronautics, Acoustics & Sound
Item Weight
17.2 Oz
Item Width
6.1 in
Number of Pages
Xiv, 198 Pages

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Product Information

Introduction 1. Method of landing aircraft using integrated satellite optical navigation system 1.1. Comparative analysis of existing instrumental landing systems, corresponding to current requirements of ICAO, and the rationale for the transition to landing an aircraft according to a satellite radio navigation system. Methods for compensating pseudorange measurement errors in a satellite radio navigation system 1.2. Development of recommendations for the use of an integrated navigation system at the approach for landing stage for various operating conditions 1.3. Methods to improve the noise immunity of the integrated navigation system in the area of the aerodrome and with an accurate approach for landing based on the optimal placement of ground equipment and three-dimensional visualization of the terrain on board of the aircraft 2. Evaluation and assurance of reliability of the navigation systems of civil aviation aircraft under the influence of various interferences 2.1. Calculation method confirming the performance and reliability of the GBAS station 2.2. The method of reducing the impact of failures of tracking of the positioning of the aircraft, arising as a result of fast maneuvering, when flying in mountainous areas and at low altitudes by optimizing the tracking system by speed 3. Methods to improve the noise immunity of the navigation system at the stage of terminal procedures and precision landing approach 3.1 Improvement of the continuity characteristics of the integrated navigation system in the area of the aerodrome and during precise landing approach based on the use of two-constellation ground-based GNSS functional aids (multi-constellation GBAS) 3.2 Improvement of the noise immunity of the integrated navigation system in the area of the aerodrome and during precise landing approach based on the use of two-constellation ground-based GNSS functional additions (multi-constellation GBAS) 3.2.1 Algorithms to ensure the noise immunity of the integrated navigation system in the area of the aerodrome by protection levels 3.2.2 Improvement of noise immunity of the integrated navigation system in the area of the aerodrome and during precise landing approach by detecting external influences on the GNSS signal 3.2.3 Detection of abnormal state of the ionosphere (ionospheric storm) 3.3 Experimental confirmation of improved navigation and landing accuracy when using ground-based local augmentation GBAS (LKKS-A-2000) of I-III category of ICAO 3.4 Metrological support of flight reviews of LKKS (GBAS) 3.5 The concept of creation and the method of implementation of the set of technical solutions of the satellite navigation and landing system (LKKS-A-2000) and the Federal GNSS Monitoring Center, which meet the modern requirements of ICAO. Results of the implementation of the proposed technical solutions 4. Improvement of noise immunity of the navigation systems of civil aircraft based on satellite and inertial navigation systems, as well as ground-based systems 4.1. Algorithm for detecting "false satellites" based on the integration of satellite and inertial navigation systems 4.2. Improvement of the noise immunity of aircraft navigation systems in subpolar latitudes based on the use of aircraft positioning devices

Product Identifiers

Publisher
Springer
ISBN-10
9811600724
ISBN-13
9789811600722
eBay Product ID (ePID)
13050393079

Product Key Features

Book Title
Modern Requirements for Noise Immunity Aircraft Navigation Equipment
Number of Pages
Xiv, 198 Pages
Language
English
Publication Year
2021
Topic
Aeronautics & Astronautics, Acoustics & Sound
Illustrator
Yes
Genre
Technology & Engineering, Science
Author
Oleg Ivanovich Zavalishin, Yury Grigoryevich Shatrakov, Dmitry Alexandrovich Zatuchny
Book Series
Springer Aerospace Technology Ser.
Format
Hardcover

Dimensions

Item Weight
17.2 Oz
Item Length
9.3 in
Item Width
6.1 in

Additional Product Features

Dewey Edition
23
Number of Volumes
1 Vol.
Dewey Decimal
629.1351
Lc Classification Number
Ta365-367.5
Table of Content
Introduction.- 1. Method of landing aircraft using integrated satellite optical navigation system.- 2. Evaluation and assurance of reliability of the navigation systems of civil aviation aircraft under the influence of various interferences.- 3. Methods to improve the noise immunity of the navigation system at the stage of terminal procedures and precision landing approach.- 4. Improvement of noise immunity of the navigation systems of civil aircraft based on satellite and inertial navigation systems, as well as ground-based systems.
Copyright Date
2021

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