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020 _a9789811026034
_q(electronic bk.)
020 _a9811026033
_q(electronic bk.)
020 _z9789811026027
020 _z9811026025
035 _a(OCoLC)961813643
_z(OCoLC)961437626
_z(OCoLC)962064806
_z(OCoLC)974651011
_z(OCoLC)981110023
_z(OCoLC)985040655
_z(OCoLC)1005787633
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_bspa
050 4 _aTL1050
_b.Y369 2017 EB
100 1 _aYan, Ye.
245 1 0 _aDynamics and control of Lorentz-augmented spacecraft relative motion
_cYe Yan, Xu Huang, Yueneng Yang.
264 1 _aSingapore
_bSpringer
264 4 _c2017.
300 _a1 recurso en línea
336 _aTexto
_btxt
_2rdacontent
337 _aelectrónico
_bc
_2rdamedia
338 _arecurso electrónico
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
500 _aSpringerLink
_bSpringer Engineering eBooks 2017 English+International
504 _aIncluye referencias bibliográficas
505 0 _aIntroduction -- Dynamical Model of Lorentz-Augmented Orbital Motion -- Relative Navigation of Lorentz-Augmented Orbital Motion -- Dynamics and Control of Lorentz-Augmented Spacecraft Hovering -- Dynamics and Control of Lorentz-Augmented Spacecraft Rendezvous -- Dynamics and Control of Lorentz-Augmented Spacecraft Formation Flying.
520 3 _aThis book develops a dynamical model of the orbital motion of Lorentz spacecraft in both unperturbed and J2-perturbed environments. It explicitly discusses three kinds of typical space missions involving relative orbital control: spacecraft hovering, rendezvous, and formation flying. Subsequently, it puts forward designs for both open-loop and closed-loop control schemes propelled or augmented by the geomagnetic Lorentz force. These control schemes are entirely novel and represent a significantly departure from previous approaches.
650 7 _aAstronáutica
_2embne
_0(OCoLC)fst00819505
_0
_9138156
700 1 _aHuang, Xu
_9100825
700 1 _aYang, Yueneng.
856 4 0 _uhttps://go.openathens.net/redirector/universidadeuropea.es?url=http://link.springer.com/10.1007/978-981-10-2603-4
_zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
988 _aEBOOK, asignarmaterias, EBSPRINGER_2017A
998 _b02/2018
_dz
_e-
_zSI
999 _c94796
_d94796
_x1