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001450900 001__ 1450900
001450900 003__ OCoLC
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001450900 019__ $$a1350469690
001450900 020__ $$a9789811963292$$q(electronic bk.)
001450900 020__ $$a9811963290$$q(electronic bk.)
001450900 020__ $$z9811963282
001450900 020__ $$z9789811963285
001450900 0247_ $$a10.1007/978-981-19-6329-2$$2doi
001450900 035__ $$aSP(OCoLC)1349567950
001450900 040__ $$aYDX$$beng$$cYDX$$dGW5XE$$dFIE$$dEBLCP$$dOCLCF$$dUKAHL$$dOCLCQ
001450900 049__ $$aISEA
001450900 050_4 $$aTL570
001450900 08204 $$a629.1323$$223/eng/20221110
001450900 1001_ $$aAkimov, Alexander Nikolaevich,$$eauthor.
001450900 24510 $$aLimiting modes of aircraft flight :$$bmethods, algorithms and results /$$cAlexander Nikolaevich Akimov, Vadim Vadimovich Vorobyov, Dmitry Alexandrovich Zatuchny.
001450900 260__ $$aSingapore :$$bSpringer,$$c2022.
001450900 300__ $$a1 online resource
001450900 336__ $$atext$$btxt$$2rdacontent
001450900 337__ $$acomputer$$bc$$2rdamedia
001450900 338__ $$aonline resource$$bcr$$2rdacarrier
001450900 4901_ $$aSpringer aerospace technology,$$x1869-1749
001450900 504__ $$aIncludes bibliographical references.
001450900 5050_ $$aIntroduction -- Chapter 1. Onboard restraint systems. State of the issue. Formulation of the problem -- Chapter 2. The method of adaptive maintenance of constraints on the components of the state vector of a dynamic system -- Chapter 3. Algorithms for adaptive limitation of aircraft flight parameters -- Chapter 4. Algorithms for adaptive limitation of trajectory parameters of aircraft movement -- Chapter 5. Aircraft drift away from limiting surfaces along programmed trajectories -- Chapter 6. Method and algorithms for direct optimization of the movement of a damaged aircraft.
001450900 506__ $$aAccess limited to authorized users.
001450900 520__ $$aThis book describes in detail a method of direct optimization, which makes it possible to choose the best trajectory of an aircraft in conditions of its limited resource. This can happen in the event of an emergency on board, associated with both a possible equipment failure and external influences, for example, when lightning strikes an aircraft or collides with a moving object. The highlight of this book is the fact that the results presented in it can be applied universally to the choice of the flight path of large and small aircraft, as well as helicopter technology. In addition, they take into account various conditions of aircraft flight, including a possible accident. The methods and algorithms presented here can be used as the basis for the creation of automatic collision avoidance systems, as well as the choice of the best aircraft trajectory for flights in different regions and in different conditions.
001450900 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed November 10, 2022).
001450900 650_0 $$aAerodynamics.
001450900 650_0 $$aFlight engineering.
001450900 650_0 $$aAirplanes$$xControl systems.
001450900 650_0 $$aAircraft accidents.
001450900 655_0 $$aElectronic books.
001450900 7001_ $$aVorobyov, Vadim Vadimovich,$$eauthor.
001450900 7001_ $$aZatuchny, Dmitry Alexandrovich,$$eauthor.
001450900 77608 $$iPrint version: $$z9811963282$$z9789811963285$$w(OCoLC)1337924529
001450900 830_0 $$aSpringer aerospace technology,$$x1869-1749
001450900 852__ $$bebk
001450900 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-981-19-6329-2$$zOnline Access$$91397441.1
001450900 909CO $$ooai:library.usi.edu:1450900$$pGLOBAL_SET
001450900 980__ $$aBIB
001450900 980__ $$aEBOOK
001450900 982__ $$aEbook
001450900 983__ $$aOnline
001450900 994__ $$a92$$bISE