000			01425nam a22002417a 4500
003			CO-NeUS
005			20180209100542.0
008			150706s2010 xxua f |||| 001 0 eng d
020			_a9780521518505
040			_aCO-NeUS _bEspañol
041			_aeng
082	0	4	_a629.411 _bS732s
245	0	0	_aSpacecrarft trajectory optimization _ceditado por Bruce A. Conway
264			_aNew York _bCambridge University Press _c2010
300			_axi, 298 páginas _bilustraciones _c25 cm.
504			_aIncluye referencias bibliográficas e índice.
505	0		_aThe problem of spaceraft trajectory optimization -- Primer vector theory and applications -- Spacecraft trajectory optimization using direct transcription and nonlinear programming -- Elements of a software system for spacecraft trajectory optimization -- Low-thrust trajectory optimization using orbital averaging and control parameterization -- Analytic representations of optimal low-thrust transfer in circular orbit -- Global optimization and space pruning for spacecraft trajectory design -- Incremental techniques for global space trajectory design -- Optimal low-thrust trajectories using stable manifolds -- Swarming theory applied to space trajectory optimization.
650	1	7	_aModelos matematicos _9116781
650	2	7	_aProgramacion lineal _9128951
650	2	7	_aTecnologia _xIngeniería _9132768
700			_aConway, Bruce A. _eeditor _937727
942			_cCG
999			_c38553 _d38553