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Limiting Modes of Aircraft Flight: Methods, Algorithms and Results: Springer Aerospace Technology

Autor Alexander Nikolaevich Akimov, Vadim Vadimovich Vorobyov, Dmitry Alexandrovich Zatuchny
en Limba Engleză Hardback – noi 2022
This book describes in detail a method of direct optimization, which makes it possible to choose the best trajectory of an aircraft in conditions of its limited resource. This can happen in the event of an emergency on board, associated with both a possible equipment failure and external influences, for example, when lightning strikes an aircraft or collides with a moving object. The highlight of this book is the fact that the results presented in it can be applied universally to the choice of the flight path of large and small aircraft, as well as helicopter technology. In addition, they take into account various conditions of aircraft flight, including a possible accident. The methods and algorithms presented here can be used as the basis for the creation of automatic collision avoidance systems, as well as the choice of the best aircraft trajectory for flights in different regions and in different conditions.
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Specificații

ISBN-13: 9789811963285
ISBN-10: 9811963282
Pagini: 174
Ilustrații: XI, 174 p. 124 illus., 2 illus. in color.
Dimensiuni: 155 x 235 mm
Greutate: 0.45 kg
Ediția:1st ed. 2022
Editura: Springer Nature Singapore
Colecția Springer
Seria Springer Aerospace Technology

Locul publicării:Singapore, Singapore

Cuprins

Introduction.- Chapter 1. Onboard restraint systems. State of the issue. Formulation of the problem.- Chapter 2. The method of adaptive maintenance of constraints on the components of the state vector of a dynamic system.- Chapter 3. Algorithms for adaptive limitation of aircraft flight parameters.- Chapter 4. Algorithms for adaptive limitation of trajectory parameters of aircraft movement.- Chapter 5. Aircraft drift away from limiting surfaces along programmed trajectories.- Chapter 6. Method and algorithms for direct optimization of the movement of a damaged aircraft.

Notă biografică

Alexander Nikolaevich Akimov is Doctor of technical sciences, Professor and Professor of the Department of Flight Safety and Life of Moscow State technical university of civil aviation and chief specialist of PJSC Sukhoi Company. He graduated from Air Force Academy named after N.E. Zhukovsky in 1981. He defended his doctoral dissertation in 1997. He is Member of Dissertation Councils. His research interests are in the areas of military cybernetics, systems analysis, operations research, systems modeling, weapons and military equipment, and military complexes and systems.
Vadim Vadimovich Vorobyev is Doctor of technical sciences, Professor and Head of the Department of Flight Safety and Life of Moscow state technical university of civil aviation. He is the author of over 130 scientific works, including 3 monographs, 2 textbooks. He is/was a scientific supervisor in the implementation of more than 30 scientific research works on issues ensuring the safety of aircraft flights in normal and special flight situations.
Dmitry Alexandrovich Zatuchny is Doctor of technical sciences, Associate Professor and Professor in 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 an 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.


Textul de pe ultima copertă

This book describes in detail a method of direct optimization, which makes it possible to choose the best trajectory of an aircraft in conditions of its limited resource. This can happen in the event of an emergency on board, associated with both a possible equipment failure and external influences, for example, when lightning strikes an aircraft or collides with a moving object. The highlight of this book is the fact that the results presented in it can be applied universally to the choice of the flight path of large and small aircraft, as well as helicopter technology. In addition, they take into account various conditions of aircraft flight, including a possible accident. The methods and algorithms presented here can be used as the basis for the creation of automatic collision avoidance systems, as well as the choice of the best aircraft trajectory for flights in different regions and in different conditions.


Caracteristici

Describes an optimization method making it possible to choose the best trajectory of an aircraft Includes algorithms for limiting the trajectory parameters of the movement of an aircraft Presents algorithms for calculating the angles of an aircraft position in space when moving away from an obstacle