000			03234nam a22004215i 4500
710	2		_aSpringerLink (Online service) _9106996
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005			20230102113444.0
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008			181220s2019 gw a o |||| 0|eng d
020			_a9783030037895
024	7		_a10.1007/978-3-030-03789-5 _2doi
040			_bspa _dES-MaUEC _cES-MaUEC
050		4	_aTL1065 _b2019 EB
100	1		_aTewari, Ashish _eautor _948596
245	1	0	_aOptimal Space Flight Navigation : _bAn Analytical Approach _cby Ashish Tewari
264		1	_aCham _bSpringer International Publishing : _bImprint: Birkhäuser _c2019
300			_a1 recurso en línea (XI, 270 páginas) _b65 ilustraciones a color
336			_2rdacontent _aTexto _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
347			_atext file _bPDF
490	0		_aControl Engineering _x2373-7719
490	0		_aEngineering (Springer-11647)
505	0		_a1. Introduction -- 2. Analytical Optimal Control -- 3. Orbital Mechanics and Impulsive Transfer -- 4. Two-Body Maneuvers with Unbounded Continuous Inputs -- 5. Optimal Maneuvers with Bounded Inputs -- 6. Flight in Non-spherical Gravity Fields.
520	3		_aThis book consolidates decades of knowledge on space flight navigation theory, which has thus far been spread across various research articles. By gathering this research into a single text, it will be more accessible to students curious about the study of space flight navigation. Books on optimal control theory and orbital mechanics have not adequately explored the field of space flight navigation theory until this point. The opening chapters introduce essential concepts within optimal control theory, such as the optimization of static systems, special boundary conditions, and dynamic equality constraints. An analytical approach is focused on throughout, as opposed to computational. The result is a book that emphasizes simplicity and practicability, which makes it accessible and engaging. This holds true in later chapters that involve orbital mechanics, two-body maneuvers, bounded inputs, and flight in non-spherical gravity fields. The intended audience is primarily upper-undergraduate students, graduate students, and researchers of aerospace, mechanical, and/or electrical engineering. It will be especially valuable to those with interests in spacecraft dynamics and control. Readers should be familiar with basic dynamics and modern control theory. Additionally, a knowledge of linear algebra, variational methods, and ordinary differential equations is recommended.
650		7	_2embne _9139696 _aVehículos espaciales
650		7	_2embne _aExploración espacial _9150923
650		7	_2embne _aAstronáutica _9138156
776	0	8	_iPrinted edition: _z9783030037888
776	0	8	_iPrinted edition: _z9783030037901
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-030-03789-5 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
988			_aPrimersemestre_2019_Engineering
998			_aSI _cm _dz _feng _ggw _h0 _b09/2019 _eel _zSI