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Information Support and Aircraft Flight Management
Oleg Ivanovich Zavalishin, Anatoly Nikolaevich Korotonoshko, Dmitry Alexandrovich Zatuchny, Yury Grigorievich Shatrakov
132,95 €
+ 265 points
Description
Introduction
Implementation and ways to implement ADS-b in Russian Federation
The implementation options for ADS
Technical implementation means ADS-b
Principles of construction of systems of ADS-b ICAO
Multifunctional channels of systems ADS-b and methods of management
Ground station VDL-4 intended for the operation of the system ADS-b
Russian information system based on ADS-b for the flight of aircraft in the Arctic and far Eastern regions
The objectives and main approaches for the development of communication and cooperation in the Arctic.
The variant of construction of the system of the Arctic ADS-b. System relay information
Communications system of the control tower - radar in shortwave range
The Russian information system of controlling the movement of aircraft in the area of the Kuril archipelago (RISCM-KA)
The objectives and main approaches to the creation of information system of RISCM-KA
Questions of technical implementation of RISCM-KA
The extension of possibilities of application of technology ADS-b in information systems of the transport complex of the Russian Federation
System ADS-b to provide a small aircraft flying in uncontrolled airspace
ADS-b in the system of transport logistics (STL) agricultural production
Control a swarm of unmanned aerial vehicles (UAVs) using the technology of ADS-b
The program of implementation tools broadcast automatic dependent surveillance in the Russian Federation
Chapter 1 Literature
Building a better computing unit for devices of civil aviation on the criterion of reliability
Development of methods of calculation of reliability computing unit, composed of heterogeneous elements
The general approach to calculation of reliability computing unit
Review of existing civil aviation computing units in the example of the aircraft "Sukhoi Superjet-100."
A formal approach to the calculation of the reliability computing unit
The method of calculating the reliability computing unit, taking into account different types of errors
Building a better computer system from heterogeneous elements according to the proposed criterion
Analysis of different approaches to the choice of the criterion to build a better system
Building the best computing unit from relay elements with possible errors of the first and second kind
Build the best multifunctional computing unit
The construction algorithm select the best computational unit based on the execution of several functions
Building a better computing device for modeling the spatial movement of the helicopter
Chapter 2 Literature
Ensuring the reliability and integrity of the information service of aircraft at various stages and under various flight conditions
The implementation of the information service of aircraft based on satellite and optical systems, designed "NPPF Spectr"
Monitoring center of satellite constellations for aviation users
Local monitoring and correcting station GBAS LCCS-A-2000
Certified small satellite tracker
Aviation satellite optical engine precise positioning the PILOT
Ground and flight checks
Spécifications
Parties prenantes
- Auteur(s) :
- Editeur:
Contenu
- Nombre de pages :
- 146
- Langue:
- Anglais
- Collection :
Caractéristiques
- EAN:
- 9789811600906
- Date de parution :
- 29-03-22
- Format:
- Livre broché
- Format numérique:
- Trade paperback (VS)
- Dimensions :
- 156 mm x 234 mm
- Poids :
- 235 g
