Development of Navigation Technology for Flight Safety

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