Conditional Function Control of Aircraft

Introduction
Contents
Abbreviations
1 Analysis of the Problem Functioning Modeling Ergatic Air Traffic Management Information System
	1.1 State of the Security Problem and Traffic Management Aircraft in the Area of the Aerodrome
	1.2 A Modern Approach to the System-Dynamic Description of an Ergatic System Functioning
	1.3 Theoretical-Multiple Model of Information Interaction of Air Traffic Control Ergatic Information System Elements
	1.4 Presentation of Informational Interaction Ergatic Elements in an Ergatic Information System
	1.5 Logical–Linguistic Model for Choosing an Analytical Model Parry Adverse Effects for Ergatic Elements
	1.6 Synthesis of a Procedural Model for Decision-Making by an Ergatic Element in the Formation of an Aircraft Stream
	1.7 The Method of Models for the Representation Synthesis of Ergatic Elements in an Ergatic Information System
	References
2 The Methodology of Functional Control of the Aircraft and Parrying Special Situations
	2.1 Analysis of Aircraft Failures and Malfunctions by Aviation Systems and Groups of Causes
	2.2 Decision-Making Model for Parrying Special Situations Onboard an Aircraft
	2.3 Methods of Functional Monitoring of the State of the Aircraft and the Organization of Information Support for Decision-Making in Special Situations
	2.4 A Model of the Functioning of the Information Support System for Decision-Making of the Aircraft Crew in a Particular Situation
	References
3 The Architecture of Safety Flights System in the Airspace of the Russian Federation
	3.1 The Role and Place of the Decision Support Information System in the Structure of the Ergatic System “Aircraft–Crew,” “Aircraft–Operator of an Unmanned Aerial Vehicle”
	3.2 Development of the Russian Federation Safety System Architecture in the Airspace
	3.3 A Model for the Optimal Placement of Critical Information Entities in a Unified Safety System
	3.4 The Concept of the Creation and Development of the Air Navigation System of Russia
	References
4 A Mathematical Model for Constructing a Conflict-Free Flow of Aircraft in the Zone of the Near Zone Officer Responsibility (Circle Dispatcher)
	4.1 Features of Information Support During the Formation of the Flow of Aircraft During Approach
	4.2 Justification of the Need to Develop a Method and Models for Organizing Information Support for the Near Zone Officer (Circle Dispatcher) in the Detection and Resolution of Potential Conflict Situations
	4.3 Determination of the Space and Trajectories of the Aircraft During Approach Conflict-Free Flow Formation
	4.4 A Model for Constructing an Aircraft Delay Maneuver for a Given Interval
	4.5 The Method of Organizing Information Support for the Near Zone Officer (Circle Dispatcher) in the Detection and Resolution of Potential Conflict Situations
		4.5.1 Description of the Method of Organizing Information Support for the Officer of the Near Zone (Circle Dispatcher) When Detecting and Resolving Potential Conflict Situations Between Aircraft Landing
		4.5.2 Organization of Information Support for the Officer of the Near Zone (Circle Dispatcher) When Forming the Aircraft Queue Without Priority
		4.5.3 Organization of Information Support for the Near Zone Officer (Circle Dispatcher) in the Formation of the Queue of Aircraft with a Priority of Service at the Incoming Aircraft
		4.5.4 Organization of Information Support for the Officer of the Near Zone (Circle Dispatcher) When Forming a Queue of Aircraft with a Priority of Service and Taking into Account Fuel Residues Onboard Each Aircraft
	References
5 Formation of Solutions for Optimizing the Activities of the Landing Zone Officer (Landing Dispatcher)
	5.1 Building a Model of a Guaranteed Aircraft Landing Approach
	5.2 Defining a Set of Safe Approach Paths
	5.3 Determining the Optimal Safe Approach Path
	5.4 A Mathematical Model for Constructing an Optimal Approach Path
		5.4.1 The Principle of Maximum Performance in Solving the Problem of Parrying Deviations from the Landing Course
		5.4.2 Aircraft Movement Model During Approach for Landing with a Decrease in Speed and Two Turns
		5.4.3 Aircraft Double Turn Modeling
	5.5 Development of a Set of Problem-Oriented Programs and Simulation Confidence Assessment
	5.6 Assessment of the Complexity of the Algorithmic Ensure of the System Decision-Making Support for the Workstation of the Landing Zone Officer (Landing Dispatcher)
	5.7 Construction of a Landing Approach Zone and Recommendations to the Officer of the Landing Zone (Landing Dispatcher) on Aircraft Control Using the Decision Support System
	5.8 Software Development of a Decision Support System for an Automated Workstation of a Landing Zone Officer (Landing Dispatcher)
	5.9 Reliability Assessment of the Model for Constructing an Optimal Approach Trajectory
	5.10 Development Of The Technology For The Operation Of Air Traffic Control (Flight Control) Service Dispatchers During Flights In Special Conditions And Individual Cases In Flight
	References