GENERAL DESCRIPTION OF FLIGHT SAFETY PROBLEMS
Analysis of the state and prospects for the development of instrument landing systems and collision avoidance systems Features of global navigation satellite systems as an instrument basis for improving flight safety
Augmentations - the main method to improve the performance characteristics of global navigation satellite systems
Analysis of requirements for satellite-based landing systems and collision avoidance systems General methods and techniques to improve flight efficiency and safety when using satellite-based landing systems and collision avoidance systems
Flight safety indicators Conclusions to Chapter 1
METHODOLOGY FOR CONSTRUCTING SATELLITE-BASED LANDING SYSTEMS AND COLLISION AVOIDANCE SYSTEMS Theoretical background of a formalized methodological approach to the selection of basic elements for radio-electronic complexes to improve flight efficiency and safety Methods for building the structure of the ground and onboard radio-electronic complexes of satellite-based landing systems with augmentations of global navigation satellite systems
Methods and rules for the development of a collision avoidance system with the use of global navigation satellite system technologies
Directions and methods to enhance satellite-based landing systems and collision avoidance systems Conclusions to Chapter 2
METHODS FOR IMPROVING FLIGHT EFFICIENCY AND SAFETY FOR SATELLITE-BASED LANDING SYSTEMS
Method for increasing the accuracy and integrity of the guidance signals based on the construction and use of volumetric distribution diagrams for radio waves multipath errors and the system structure for its implementation
Method for ensuring integrity and continuity of guidance signals based on the use of an integrated signal-to-noise ratio for pseudoranges in presence of radiointerference
Method for increasing accuracy and integrity of guidance signals based on pseudorange error compensation using phase measurements and the structure of the radioelectronic complex for its implementation
Method for increasing accuracy, integrity, continuity and availability of guidance signals based on the use of pseudo-satellite signals and the system structure for its implementation
Conclusions to Chapter 3
METHODS FOR IMPROVING FLIGHT EFFICIENCY AND SAFETY BASED ON TECHNOLOGIES APPLICABLE IN COLLISION AVOIDANCE SYSTEMS
Method for improving flight safety by generating a warning about a potential collision based on the three-dimensional synthesis of the underlying surface sections and the display of hazardous elements
Method for increasing the flight effectiveness and safety by assessing the possibility of vertical maneuvering and determining the direction of the turn
Method for increasing the flight effectiveness and safety by identifying hazardous terrain, taking into account the possibility of a reverse turn, and the system structure for its implementation Method for improving flight efficiency and safety by analyzing the space inside a corridor safe for flight
Conclusions to Chapter 4
INTEGRATED TECHNICAL SOLUTIONS ON THE JOINT USE OF TECHNOLOGIES APPLICABLE IN COLLISION AVOIDANCE SYSTEMS AND SATELLITE-BASED LANDING SYSTEMS
Principles of constructing an integrated flight safety enhancement system based on the collision avoidance system and the satellite-based landing system
About the Author:
Baburov Sergey Vladimirovich, Candidate of Technical Sciences, was born in 1984. He is the author of more than 82 scientific papers, including 4 patents for inventions in the field of radio technical systems; expert in the field of system analysis, on-board radio communication systems, navigation and air traffic control; First Deputy General Director of JSC "Navigator" for the development and production of a wide range of on-board integrated avionics.
Bestugin Alexander Roaldovich, Professor, Doctor of Technical Sciences, was born in 1960. He is the Director of the St. Petersburg State University of Aerospace Instrumentation Second Institute, Head of the "Design Process for Electronic and Laser aids" Department, author of more than 100 scientific papers, including 11 monographs, 4 patents for inventions in the field of radio technical aids, research supervisor of the section for multifunctional aircraft flight control systems.
Galyamov Andrey Mikhailovich, Candidate of Technical Sciences, was born in 1987. He is the author of more than 50 scientific papers, including 2 patents for inventions in the field of radio technical systems; General Director of NNC Consulting LLC, Interstate Aviation Committee expert-auditor, Rosaviation expert-auditor, Head of the testing laboratory, RTCA and EUROCAE member, expert in testing radio-electronic complexes and improving flight safety for all types of aircraft.
Sauta Oleg Ivanovich, Doctor of Technical Sciences, was born in 1960. He is the author of more than 100 scientific papers, including 20 patents for inventions in the field of radio technical systems for satellite navigation, landing and safety enhancement systems. He graduated from Leningrad State University, specializing in radiophysics (1983). He defended his candidate thesis in 1991 and doctoral thesis in 2012. He is an expert in the field of aviation radio technical systems for navigation and landing, founder of the scientific field of ergatic complexes for displaying navigational information and external environment for improving flight safety and reducing the meteorological minimum. He is the Deputy Chief Designer of the first Russian series-produced on-board ground proximity warning systems and satellite-based landing systems for all types of aircraft.
Shatrakov Yury Grigorievich, Professor, Doctor of Technical Sciences, Honored Science Worker of Russia, Laureate of State and St. Petersburg Government Prizes, RATS full member, graduated from Leningrad Institute of Aviation Instrumentation and Leningrad University (Physics and Mathematics Faculty). He was a full-time postgraduate student at All-Russian Scientific Research Institute of Radio Equipment. He defended his thesis in 1966. He published 52 monographs and textbooks on radio navigation, radiolocation, production organization. He prepared more than 100 candidates and doctors of science as a scientific adviser and scientific consultant. Scientific directions founded under the guidance of Yu.G. Shatrakov are as follows: relative radio navigation; increased noise immunity of angle measuring systems due to suppression of correlation errors and interference; secondary radiolocation by individual numbers; reduction of labor intensity in the production of radio electronic products due to the introduction of flexible automated productions. He is the author of more than 400 scientific works, including 30 patents for inventions in the field of radio technical systems; Head of the industry (45 enterprises and research institutes) for the creation of navigation, landing and ATM (1978-1988) aids; scientific supervisor of international projects for the creation of the MLS with Thomson-CSF (1980-1988), with US enterprises for the creation of joint LRNSs (long-range radio technical navigation systems) (Tropic-Loran) (1984), chief designer of on-board antenna-feed systems; founder of the correlation interference theory in aviation radio technical complexes and systems.
