000			03250nam a22004095i 4500
001			85111
003			ES-MaUEC
005			20230207040456.0
007			cr nn 008mamaa
008			151027s2016 gw a s 001 0 eng d
020			_a9783319255408
024	7		_a10.1007/978-3-319-25540-8 _2doi
040			_aES-MaUEC
050		4	_aTL500 _b.M39 2016 EB
082	0	4	_a629.1
100	1		_aMazzini, Leonardo _997829 _0Local
245	1	0	_aFlexible Spacecraft Dynamics, Control and Guidance : _bTechnologies by Giovanni Campolo _cby Leonardo Mazzini
250			_a1st ed.
264		1	_aCham _bSpringer International Publishing _c2016
300			_a1 recurso en línea (XXI, 363 p.) _b154 ilustraciones, 20 ilustraciones en color
336			_aTexto (visual) _btxt _2rdacontent
337			_aelectrónico _bc _2rdamedia
338			_arecurso electrónico _bcr _2rdacarrier
490	1		_aSpringer Aerospace Technology _x1869-1730
505	0		_aIntroduction -- The Kinematic of the flexible satellite -- The Satellite Attitude Control System -- The Dynamic of the flexible body -- The Dynamic in the Gravitational Field -- The Optimal Control Theory -- Attitude Control Methods -- Orbital Dynamic and Control -- Spacecraft Propulsion -- Sensors and Actuators technologies -- Complements to Body Kinematic -- Elements of Estimation Theory -- Basics of Lagrangian Equations -- The J2 perturbation solution -- Complements to Optimal Orbital Transfer -- Elements of Plasma physics.
520	3		_aThis book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers. After an introduction on the kinematics of the flexible and agile space vehicles, the modern architecture and functions of an AOC system are described and the main AOC modes reviewed with possible design solutions and examples. The dynamics of the flexible body in space are then considered using an original Lagrangian approach suitable for the control applications of large space flexible structures. Subsequent chapters address optimal control theory, attitude control methods, and orbit control applications, including the optimal orbital transfer with finite and infinite thrust. The theory is integrated with a description of current propulsion systems, with the focus especially on the new electric propulsion systems and state of the art sensors and actuators.
710	2		_aSpringerLink (Online service) _0Local _9106996
942			_2lcc _cLE
988			_aEBOOK, EBSPRINGER
650		7	_aAstronáutica _0comprobar BNE19900956291 _2embne _9138156
830		0	_aSpringer Aerospace Technology _x1869-1730 _9134166
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://link.springer.com/book/10.1007/978-3-319-25540-8 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
901			_ai9783319255408
907			_a.b12943897 _b10-10-17 _c21-11-16
998			_am _a_alco _a_vill _b29-09-17 _cm _dz _ei _feng _ggw _h0
945			_aTL500 .M39 2016 EB _g1 _ieBOOK _j0 _lmae _o- _pEUR0.00 _q- _r- _sb _t15 _u0 _v0 _w0 _x0 _y.i11588044 _z06-04-17
999			_c85111 _d85111 _x1