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Limiting modes of aircraft flight = ...

Akimov, Alexander Nikolaevich.

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Limiting modes of aircraft flight = methods, algorithms and results /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Limiting modes of aircraft flight/ by Alexander Nikolaevich Akimov, Vadim Vadimovich Vorobyov, Dmitry Alexandrovich Zatuchny.
其他題名:	methods, algorithms and results /
作者:	Akimov, Alexander Nikolaevich.
其他作者:	Vorobyov, Vadim Vadimovich.
出版者:	Singapore :Springer Nature Singapore : : 2022.,
面頁冊數:	xi, 174 p. :ill., digital ;24 cm.
內容註:	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.
Contained By:	Springer Nature eBook
標題:	Aerodynamics. -
電子資源:	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 flightmethods, algorithms and results /[electronic resource] :by Alexander Nikolaevich Akimov, Vadim Vadimovich Vorobyov, Dmitry Alexandrovich Zatuchny. - Singapore :Springer Nature Singapore :2022. - xi, 174 p. :ill., digital ;24 cm. - 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:

532569
Aerodynamics.

LC Class. No.: TL570 / .A55 2022

Dewey Class. No.: 629.1323

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520 $a 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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