Hamiltonian perturbation solutions for spacecraft orbit prediction: the method of lie transforms

Analytical solutions to the orbital motion of celestial objects have been nowadays mostly replaced by numerical solutions, but they are still irreplaceable whenever speed is to be preferred to accuracy, or to simplify a dynamical model. In this book, the most common orbital perturbations problems ar...

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Bibliographic Details
Main Author: Lara, Martín (Author)
Format: Electronic eBook
Language:English
Published: Berlin ; Boston De Gruyter [2021]
Series:De Gruyter Studies in Mathematical Physics 54
Subjects:
Online Access:DE-1043
DE-1046
DE-858
DE-859
DE-860
DE-355
DE-739
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Summary:Analytical solutions to the orbital motion of celestial objects have been nowadays mostly replaced by numerical solutions, but they are still irreplaceable whenever speed is to be preferred to accuracy, or to simplify a dynamical model. In this book, the most common orbital perturbations problems are discussed according to the Lie transforms method, which is the de facto standard in analytical orbital motion calculations
Item Description:Description based on online resource; title from PDF title page (publisher's Web site, viewed 26. Mai 2021)
Physical Description:1 Online-Ressource (XVI, 378 Seiten)
ISBN:9783110668513
DOI:10.1515/9783110668513

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