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008			200513s2020 gw a o |||| 0|eng d
020			_a9783030473488
024	7		_a10.1007/978-3-030-47348-8 _2doi
040			_aES-MaUEC _bspa _cES-MaUEC _dES-MaUEC
050		4	_aUG630 _b2020 EB
100	1		_aHe, Shaoming _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _0http://id.loc.gov/authorities/names/n2017024615 _1http://viaf.org/viaf/6897149416769989730000 _9675784
245	1	0	_aOptimal Guidance and Its Applications in Missiles and UAVs / _cShaoming He, Chang-Hun Lee, Hyo-Sang Shin, Antonios Tsourdos
250			_aFirst edition
264		1	_aCham _bSpringer International Publishing : _bImprint: Springer _c2020
300			_a1 recurso en línea (XIII, 214 páginas) _b49 ilustraciones, 47 ilustraciones a color
336			_2rdacontent _aTexto _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
347			_aArchivo de texto _bPDF
490	0		_aSpringer Aerospace Technology _x1869-1730
490	0		_aEngineering (Springer-11647)
505	0		_aIntroduction of Optimal Guidance -- Optimality of Error Dynamics in Missile Guidance -- Three-Dimensional Optimal Impact-Time-Control Guidance Law -- Gravity-Turn Assisted Optimal Guidance Law -- Observability-Enhancement Optimal Guidance Law -- Optimal Proportional-Integral Guidance Law -- Energy-Optimal Waypoint-Following Guidance Law -- Conclusions.
520	3		_aThis book presents a comprehensive overview of the recent advances in the domain of optimal guidance, exploring the characteristics of various optimal guidance algorithms and their pros and cons. Optimal guidance is based on the concept of trajectory optimization, which minimizes the meaningful performance index while satisfying certain terminal constraints, and by properly designing the cost function the guidance command can serve as a desired pattern for a variety of mission objectives. The book allows readers to gain a deeper understanding of how optimal guidance law can be utilized to achieve different mission objectives for missiles and UAVs, and also explores the physical meaning and working principle of different new optimal guidance laws. In practice, this information is important in ensuring confidence in the performance and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority.
988			_aSpringer_Engineering_23062020
650		7	_aAviación _2embne _9682652
650		7	_aMisiles _2embne _9671218
650		7	_aDrones _xSistemas de control _2embne _9667210
700	1		_aLee, Chang-Hun _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _9675787
700	1		_aShin, Hyo-Sang _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _1http://viaf.org/viaf/314929546 _9675788
700	1		_aTsourdos, Antonios _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _0http://id.loc.gov/authorities/names/n2010044169 _1http://viaf.org/viaf/273214309 _9675789
710	2		_aSpringerLink (Online service) _0http://id.loc.gov/authorities/names/no2005046756 _1http://viaf.org/viaf/148105729
776	0	8	_iPrinted edition: _z9783030473471
776	0	8	_iPrinted edition: _z9783030473495
776	0	8	_iPrinted edition: _z9783030473501
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-030-47348-8 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_b09/2020 _dz _eo _zSI