A mathematical perspective on flight dynamics and control

This brief presents several aspects of flight dynamics, which are usually omitted or briefly mentioned in textbooks, in a concise, self-contained, and rigorous manner. The kinematic and dynamic equations of an aircraft are derived starting from the notion of the derivative of a vector and then thoro...

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Bibliographic Details
Main Author: L'Afflitto, Andrea, (Author)
Format: eBook
Language: English
Published: Cham : Springer, 2017.
Series: SpringerBriefs in applied sciences and technology.
Subjects:
Aerodynamics > Mathematics.
Flight control > Mathematics.
elektronické knihy
electronic books
ISBN: 9783319474670
9783319474663
Physical Description: 1 online resource

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100 1 |a L'Afflitto, Andrea,  |e author. 
245 1 2 |a A mathematical perspective on flight dynamics and control /  |c Andrea L'Afflitto. 
264 1 |a Cham :  |b Springer,  |c 2017. 
300 |a 1 online resource 
336 |a text  |b txt  |2 rdacontent 
337 |a počítač  |b c  |2 rdamedia 
338 |a online zdroj  |b cr  |2 rdacarrier 
490 1 |a Springer briefs in applied sciences and technology 
504 |a Includes bibliographical references. 
505 0 |a Fundamentals of Rigid-Body Dynamics -- Equations of Motion of an Aircraft -- Aircraft Automatic Control -- Conclusion -- Appendix: Fundamentals of Dynamical Systems Theory. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 |a This brief presents several aspects of flight dynamics, which are usually omitted or briefly mentioned in textbooks, in a concise, self-contained, and rigorous manner. The kinematic and dynamic equations of an aircraft are derived starting from the notion of the derivative of a vector and then thoroughly analysed, interpreting their deep meaning from a mathematical standpoint and without relying on physical intuition. Moreover, some classic and advanced control design techniques are presented and illustrated with meaningful examples. Distinguishing features that characterize this brief include a definition of angular velocity, which leaves no room for ambiguities, an improvement on traditional definitions based on infinitesimal variations. Quaternion algebra, Euler parameters, and their role in capturing the dynamics of an aircraft are discussed in great detail. After having analyzed the longitudinal- and lateral-directional modes of an aircraft, the linear-quadratic regulator, the linear-quadratic Gaussian regulator, a state-feedback H-infinity optimal control scheme, and model reference adaptive control law are applied to aircraft control problems. To complete the brief, an appendix provides a compendium of the mathematical tools needed to comprehend the material presented in this brief and presents several advanced topics, such as the notion of semistability, the Smith?McMillan form of a transfer function, and the differentiation of complex functions: advanced control-theoretic ideas helpful in the analysis presented in the body of the brief. A Mathematical Perspective on Flight Dynamics and Control will give researchers and graduate students in aerospace control an alternative, mathematically rigorous means of approaching their subject. 
590 |a SpringerLink  |b Springer Complete eBooks 
650 0 |a Aerodynamics  |x Mathematics. 
650 0 |a Flight control  |x Mathematics. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
776 0 8 |i Print version:  |a L'Afflitto, Andrea.  |t Mathematical perspective on flight dynamics and control.  |d Cham : Springer, 2017  |z 9783319474663  |z 3319474669  |w (OCoLC)958460369 
830 0 |a SpringerBriefs in applied sciences and technology. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://link.springer.com/10.1007/978-3-319-47467-0  |y Plný text 
992 |c NTK-SpringerENG 
999 |c 99780  |d 99780 
993 |x NEPOSILAT  |y EIZ 

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