04600nam a22005775i 4500 978-3-031-58476-3 DE-He213 20251030112251.0 cr nn 008mamaa 241205s2024 sz | s |||| 0|eng d 9783031584763 978-3-031-58476-3 10.1007/978-3-031-58476-3 doi TL787-4050 TTD bicssc SCI098000 bisacsh TTD thema Jochim, Ernst Friedrich Maria. author. aut http://id.loc.gov/vocabulary/relators/aut 78072 Satellite Equivalence Orbits [electronic resource] : Analysis of Orbits Combining Different Motions / by Ernst Friedrich Maria Jochim. 1st ed. 2024. Cham : Springer Nature Switzerland : Imprint: Springer, 2024. XX, 481 p. 132 illus., 129 illus. in color. online resource. text txt rdacontent computer c rdamedia online resource cr rdacarrier text file PDF rda Space Technology Library, 2542-8896 ; 42 INTRODUCTION -- 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. This 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. Outer space Exploration. 69043 Astronautics. 66336 Aerospace engineering. 66335 Astrophysics. 68037 Mechanics. 68102 Space Exploration and Astronautics. 69044 Aerospace Technology and Astronautics. 66339 Astrophysics. 68037 Classical Mechanics. 68103 SpringerLink (Online service) Springer Nature eBook Printed edition: 9783031584756 Printed edition: 9783031584770 Printed edition: 9783031584787 Space Technology Library, 2542-8896 ; 42 78073 https://doi.org/10.1007/978-3-031-58476-3 ZDB-2-PHA ZDB-2-SXP 60422 60422