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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Библиографическая информация
Главный автор: Lara, Martín
Формат: Электронная книга
Язык:English
Публикация: Berlin ; Boston Walter de Gruyter GmbH, [2021]
Серии:De Gruyter studies in mathematical physics ; v. 54.
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Online-ссылка:https://www.lib.tsu.ru/mminfo/2023/EBSCO/2907461.pdf