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Conditional Function Control of Aircraft, 1st ed. 2021 Springer Aerospace Technology Series

Langue : Anglais

Auteurs :

Couverture de l’ouvrage Conditional Function Control of Aircraft
This book highlights the prevention of possible accidents and crashes of aircrafts by analyzing the many factors that affect such events. It includes the theoretical study of known ideas and concepts, as well as a set of new methods and mathematical models. It contains factual information to investigate famous disasters and aviation accidents with aircrafts. The book proposes methods and models that can be the basis in developing guidance material for decision-making by the flight crew and experts in air traffic control. Some of the contents presented in this book are also useful in the design and operation of data transmission systems of aircraft. The book is intended for engineering and technical specialists engaged in the development, manufacturing and operations of onboard radio electronic systems of aircraft and ground-based radio engineering support for flights, as well as graduate students and senior students of radio engineering specialties. It is useful to researchers and managers whose activities are related to air traffic control.

Introduction

1. Analysis of the state of the problem of modeling functioning ergatic air traffic management information system

1.1. The state of the security problem and traffic management aircraft in the area of the aerodrome

1.2. A modern approach to the systematic dynamic description of the functioning of an ergatic system

1.3. Set-theoretic model of information interaction of the elements of the ergatic information system of air traffic control

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 decision-making procedural model for an ergatic element during

air traffic flow arrangement

1.7. The method of synthesis of models for the representation 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 factors of causes

2.2. Decision-making model for parrying special situations on board 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 the safety 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 architecture of a safety system in the airspace of the Russian Federation

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. The mathematical model for building a conflict-free flow of aircraft in the zone of responsibility of the officer of the near zone

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 officer of the near zone in the detection and resolution of potential conflict situations

4.3. Definition of space and formation trajectories

Conflict-free aircraft flow during an approach

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 in the detection and resolution of potential conflict situations

4.5.1. Description of the method of organizing information support for the near zone when detecting and resolving potential conflict situations between aircraft approaching

4.5.2. Organization of information support for the near zone officer when forming the queue of aircraft without a priority of service

4.5.3. Organization of information support for the near zone officer when forming a queue of aircraft with a priority of service for an incoming aircraft

4.5.4. Organization of information support for the near zone officer in the formation of the aircraft queue with the 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

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 a landing approach with a decrease in speed and two turns

5.4.3. Aircraft Double U-Turn Modeling

5.5. Development of a set of problem-oriented programs and evaluation confidence modeling

5.6. Assessment of the complexity of the algorithmic support system decision-making workstation of the landing zone officer

5.7. Construction of the approach zone and recommendations to the zone leader aircraft control landing using a decision support system

5.8. Acceptance Support System Software Development solutions for the automated workplace of the landing zone officer

5.9. Estimation of the reliability of the model for constructing an optimal approach trajectory for landing

5.10. Development of the technology for the operation of service dispatchers air traffic (flight control) during flights in special conditions and exceptional cases in flight

References

Andrey Vyacheslavovich Yakovlev is Associate Professor, Candidate of technical science and Head of the research department at the State Center for the training of aviation personnel and military tests. He graduated from the Tambov Higher Military Aviation Engineering College of Radio Electronics in 1998 with a degree in Radio Electronic Systems.  He has authored more than 120 publications, including three monographs, 10 study guides and more than 50 scientific papers, most of which are devoted to improving the tactical and technical characteristics of modern electronic systems and complexes.

Andrey Sergeevich Istomin is Candidate of technical science and Deputy Head of the research department at the State Center for the training of aviation personnel and military tests. He graduated from the Armavir Military Aviation Institute in 2001 with a degree in Command Tactical Aviation, operation of air transport, Air Force Academy.  He is the author of more than 30 publications, including 10 study guides.

Dmitry Alexandrovich Zatuchny is Doctor of technical sciences, Associate Professor and Professor at the Department of Computation Machines, Complexes, Systems and Networks at Moscow State Technical University of Civil Aviation. He is the author of more than 140 scientific works, including 5 monographs, 6 textbooks, 1 patent on invention and 6 state registered computer programs. He was responsible for a number of research projects on ensuring the functioning of modern navigation systems in civil aviation aircraft and air traffic control. 

Yury Grigorievich Shatrakov is Doctor of Technical Sciences, Professor, Russian Federation Honored Worker of Science, Professor at the Academy of Technological Sciences of the Russian Federation and Scientific secretary of JSC&n

Presents the analysis of aircraft failures and malfunctions in aviation systems and related factors

Includes a model for the functioning of the information support system in decision-making of the aircraft crew in particular situations

Highlights a method of information support in the detection and resolution of potential conflict situation

Date de parution :

Ouvrage de 143 p.

15.5x23.5 cm

Disponible chez l'éditeur (délai d'approvisionnement : 15 jours).

105,49 €

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Date de parution :

Ouvrage de 143 p.

15.5x23.5 cm

Disponible chez l'éditeur (délai d'approvisionnement : 15 jours).

147,69 €

Ajouter au panier