000			03552nam a22004935i 4500
001			978-3-540-78522-4
003			DE-He213
005			20161121230921.0
007			cr nn 008mamaa
008			100301s2008 gw | s |||| 0|eng d
020			_a9783540785224 _9978-3-540-78522-4
024	7		_a10.1007/978-3-540-78522-4 _2doi
050		4	_aQC801-809
072		7	_aPHVG _2bicssc
072		7	_aSCI032000 _2bisacsh
082	0	4	_a550 _223
082	0	4	_a526.1 _223
100	1		_aXu, Guochang. _eauthor.
245	1	0	_aOrbits _h[electronic resource] / _cby Guochang Xu.
264		1	_aBerlin, Heidelberg : _bSpringer Berlin Heidelberg, _c2008.
300			_aXVIII, 230 p. 26 illus. _bonline resource.
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
347			_atext file _bPDF _2rda
505	0		_aCoordinate and Time Systems -- Keplerian Orbits -- Perturbations on the Orbits -- Solutions of C$20$Perturbation -- Solutions of Geopotential Perturbations -- Solutions of Extraterrestrial Disturbances -- Numerical Orbit Determination -- Analytic Orbit Determination -- Singularity-Free Theory and Discussions.
520			_aThe purpose of this reference and handbook is to describe and to derive the analytic solutionsoftheequationsofsatellitemotionperturbedbyextraterrestrialandgeo- tential disturbances of the second order. The equations of satellite motion perturbed by extraterrestrial disturbances are solved by means of discretization and appr- imated potential function as well as Gaussian equations. The equations perturbed by geopotential disturbances are solved by symbolic mathematical operations. The traditional problem of singularity in the solutions is solved by so-called singulari- free orbit theory. Simpli?ed disturbed equations of motion are proposed to simplify the solutions. Applications of the theory for analytic orbit determination are also discussed. Indeed, this is the ?rst book since the satellite era, which describes s- tematically the orbit theory with analytical solutions, with respect to all of extrat- restrial and geopotential disturbances of the second order, and the solutions are free of singularity. Based on such a theory, the algorithms of orbit determination can be renewed; deeper insight into the physics of disturbances becomes possible; the way to a variety of new applications and re?nements is opened. My primary knowledge of the orbit theory came from my education of mat- matics while studying physics and theoretical mechanics (1981). My ?rst practical experience with orbit came from the research activity at the Technical University (TU) Berlin on orbit corrections of the satellite altimetry data (1988–1992). The extensive experience on orbit came from the GPS/Galileo software development for orbit determination and geopotential mapping at the GFZ (2001–2004).
650		0	_aEarth sciences.
650		0	_aGeophysics.
650		0	_aSpace sciences.
650		0	_aAerospace engineering.
650		0	_aAstronautics.
650	1	4	_aEarth Sciences.
650	2	4	_aGeophysics/Geodesy.
650	2	4	_aExtraterrestrial Physics, Space Sciences.
650	2	4	_aAerospace Technology and Astronautics.
650	2	4	_aEarth Sciences, general.
710	2		_aSpringerLink (Online service)
773	0		_tSpringer eBooks
776	0	8	_iPrinted edition: _z9783540785217
856	4	0	_uhttp://dx.doi.org/10.1007/978-3-540-78522-4
912			_aZDB-2-EES
950			_aEarth and Environmental Science (Springer-11646)
999			_c505885 _d505885