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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| Format: | eBook |
| Language: | English |
| Published: |
Berlin ; Boston
Walter de Gruyter GmbH,
[2021]
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| Series: | De Gruyter studies in mathematical physics ;
v. 54. |
| Subjects: | |
| Online Access: | https://www.lib.tsu.ru/mminfo/2023/EBSCO/2907461.pdf |
| 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. |
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| Item Description: | Description based upon print version of record. |
| Physical Description: | 1 online resource (394 pages). |
| Bibliography: | Includes bibliographical references and index. |
| ISBN: | 9783110668513 3110668513 9783110667325 3110667320 |