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Limiting Modes of Aircraft Flight = Methods, Algorithms and Results /
Record Type:
Language materials, printed : Monograph/item
Title/Author:
Limiting Modes of Aircraft Flight/ by Alexander Nikolaevich Akimov, Vadim Vadimovich Vorobyov, Dmitry Alexandrovich Zatuchny.
Reminder of title:
Methods, Algorithms and Results /
Author:
Akimov, Alexander Nikolaevich.
other author:
Vorobyov, Vadim Vadimovich.
Description:
XI, 174 p. 124 illus., 2 illus. in color.online resource. :
Contained By:
Springer Nature eBook
Subject:
Aerospace engineering. -
Online resource:
https://doi.org/10.1007/978-981-19-6329-2
ISBN:
9789811963292
Limiting Modes of Aircraft Flight = Methods, Algorithms and Results /
Akimov, Alexander Nikolaevich.
Limiting Modes of Aircraft Flight
Methods, Algorithms and Results /[electronic resource] :by Alexander Nikolaevich Akimov, Vadim Vadimovich Vorobyov, Dmitry Alexandrovich Zatuchny. - 1st ed. 2022. - XI, 174 p. 124 illus., 2 illus. in color.online resource. - Springer Aerospace Technology,1869-1749. - Springer Aerospace Technology,.
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.
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.
ISBN: 9789811963292
Standard No.: 10.1007/978-981-19-6329-2doiSubjects--Topical Terms:
686400
Aerospace engineering.
LC Class. No.: TL1-4050
Dewey Class. No.: 629.1
Limiting Modes of Aircraft Flight = Methods, Algorithms and Results /
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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.
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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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