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001 978-3-031-58476-3
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020 _a9783031584763
_9978-3-031-58476-3
024 7 _a10.1007/978-3-031-58476-3
_2doi
050 4 _aTL787-4050
072 7 _aTTD
_2bicssc
072 7 _aSCI098000
_2bisacsh
072 7 _aTTD
_2thema
100 1 _aJochim, Ernst Friedrich Maria.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_978072
245 1 0 _aSatellite Equivalence Orbits
_h[electronic resource] :
_bAnalysis of Orbits Combining Different Motions /
_cby Ernst Friedrich Maria Jochim.
250 _a1st ed. 2024.
264 1 _aCham :
_bSpringer Nature Switzerland :
_bImprint: Springer,
_c2024.
300 _aXX, 481 p. 132 illus., 129 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aSpace Technology Library,
_x2542-8896 ;
_v42
505 0 _aINTRODUCTION -- COMPILATION OF RELATED SATELLITE ORBITAL MOTIONS -- EQUIVALENCE ORBITS RELATED TO MERIDIONAL MOTION -- EQUIVALENCE ORBITS RELATED TO SUN-SYNODIC MOTION -- EQUIVALENCE ORBITS RELATED TO MOON-SYNODIC MOTION -- NEAR-PARALLEL EQUIVALENCE SATELLITE ORBITS -- MULTIPLE COUPLING OF EQUIVALENCE ORBITS -- EQUIVALENCE ORBITS RELATED TO A FIXED SATELLITE PERIOD -- COMPILATION OF SOME CHARACTERISTIC PROPERTIES OF SATELLITE -- APPENDIX -- REFERENCES -- LIST OF SYMBOLS -- INDEX.
520 _aThis book presents the essential characteristics of the different satellite motions. Satellite motions can be classified as anomalistic, draconitic, tropical, Hansen-, Kepler-, meridional, Sun-synodical, Moon-synodical motion, depending on the relevant reference point. When two of these types of motions (in some cases even more than two) are coupled, satellite orbits are obtained, which are called equivalence orbits in this book. They share the special properties of the different coupled motions and are therefore of particular interest in the selection of special satellite orbits. In the book the author calculates mean equivalence orbits with secular perturbation formulas, as well as true equivalence orbits considering a complete orbit model including periodic motion effects. Some of the equivalence orbits can be determined unambiguously and with extremely high accuracy, they are stable in the long term. Others can only be found with low accuracy and reduced stability. The author investigates all possible combinations and the associated general equations of condition are derived in each case. Some well-known families of satellite orbits, such as the Sun-synchronous orbits, can be interpreted as mean equivalence orbits. The study of their stability is of great interest in orbit mechanics. Special applications and numerous numerical examples, graphical representations of all possible ranges of the Kepler elements, and detailed studies of the stability of particularly important equivalence orbits are carried out using the Brouwer orbit model as well as the modification by Eckstein. This lays the foundation for possible refinements using arbitrary extended orbital models and for possibly required orbital corrections. Numerous problems are to deepen the treated topics and/or to stimulate for further investigations. The book will be of interest to Astrodynamics and Aerospace Engineers as well as graduate students studying satellite orbits.
650 0 _aOuter space
_xExploration.
_969043
650 0 _aAstronautics.
_966336
650 0 _aAerospace engineering.
_966335
650 0 _aAstrophysics.
_968037
650 0 _aMechanics.
_968102
650 1 4 _aSpace Exploration and Astronautics.
_969044
650 2 4 _aAerospace Technology and Astronautics.
_966339
650 2 4 _aAstrophysics.
_968037
650 2 4 _aClassical Mechanics.
_968103
710 2 _aSpringerLink (Online service)
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9783031584756
776 0 8 _iPrinted edition:
_z9783031584770
776 0 8 _iPrinted edition:
_z9783031584787
830 0 _aSpace Technology Library,
_x2542-8896 ;
_v42
_978073
856 4 0 _uhttps://doi.org/10.1007/978-3-031-58476-3
912 _aZDB-2-PHA
912 _aZDB-2-SXP
999 _c60422
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