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000779322 1001_ $$aL'Afflitto, Andrea,$$eauthor.
000779322 24512 $$aA mathematical perspective on flight dynamics and control /$$cAndrea L'Afflitto.
000779322 264_1 $$aCham :$$bSpringer,$$c2017.
000779322 300__ $$a1 online resource.
000779322 336__ $$atext$$btxt$$2rdacontent
000779322 337__ $$acomputer$$bc$$2rdamedia
000779322 338__ $$aonline resource$$bcr$$2rdacarrier
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000779322 4901_ $$aSpringer briefs in applied sciences and technology
000779322 504__ $$aIncludes bibliographical references.
000779322 5050_ $$aFundamentals of Rigid-Body Dynamics -- Equations of Motion of an Aircraft -- Aircraft Automatic Control -- Conclusion -- Appendix: Fundamentals of Dynamical Systems Theory.
000779322 506__ $$aAccess limited to authorized users.
000779322 520__ $$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.
000779322 588__ $$aOnline resource; title from PDF title page (viewed February 9, 2017)
000779322 650_0 $$aAerodynamics$$xMathematics.
000779322 650_0 $$aFlight control$$xMathematics.
000779322 77608 $$iPrint version:$$z9783319474663$$z3319474669$$w(OCoLC)958460369
000779322 830_0 $$aSpringerBriefs in applied sciences and technology.
000779322 852__ $$bebk
000779322 85640 $$3SpringerLink$$uhttps://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-3-319-47467-0$$zOnline Access$$91397441.1
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