000			03724cam a2200397Ii 4500
001			95318
003			ES-MaUEC
005			20230102112657.0
006			m o d
007			cr cnu---unuuu
008			170203s2017 sz ob 000 0 eng d
020			_a3319474677 _q(electronic bk.)
020			_a9783319474670 _q(electronic bk.)
020			_z3319474669
020			_z9783319474663
035			_a(OCoLC)971245964 _z(OCoLC)971588240 _z(OCoLC)971969498 _z(OCoLC)972152548 _z(OCoLC)972265493 _z(OCoLC)972428410 _z(OCoLC)972538610 _z(OCoLC)981775090 _z(OCoLC)1005755221 _z(OCoLC)1011995090
040			_aN$T _cN$T _dN$T _dEBLCP _dGW5XE _dIDEBK _dYDX _dNJR _dUAB _dCOO _dINU _dIOG _dAZU _dUWO _dUPM _dOCLCF _dESU _dZ5A _dJBG _dIAD _dICW _dICN _dOTZ _dOCLCQ _dVT2 _dIDB _dU3W _dMERUC _dES-MaUEC _bspa
050		4	_aTL573 _b.L344 2017 EB
100	1		_aL'Afflitto, Andrea, _eautor
245	1	2	_aA mathematical perspective on flight dynamics and control _cAndrea L'Afflitto.
264		1	_aCham _bSpringer _c2017
300			_a1 recurso en línea
336			_aTexto _btxt _2rdacontent
337			_aelectrónico _bc _2rdamedia
338			_arecurso electrónico _bcr _2rdacarrier
347			_atext file _bPDF _2rda
490	0		_aSpringer briefs in applied sciences and technology
500			_aSpringerLink _bSpringer Engineering eBooks 2017 English+International
504			_aIncluye referencias bibliográficas
505	0		_aFundamentals of Rigid-Body Dynamics -- Equations of Motion of an Aircraft -- Aircraft Automatic Control -- Conclusion -- Appendix: Fundamentals of Dynamical Systems Theory.
520	3		_aThis 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.
650		7	_aAstronáutica _2embne _0(OCoLC)fst00819505 _0 _9138156
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=http://link.springer.com/10.1007/978-3-319-47467-0 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
988			_aEBOOK, asignarmaterias, EBSPRINGER_2017B
998			_b02/2018 _dz _e- _zSI
999			_c95318 _d95318 _x1