A study of the range of validity for the method of Kryloff and Bogoliuboff as applied to a satellite in motion with a specified constant thrust
The solution to the problem of a satellite with a small constant thrust and under the influence of a central force field presents difficulties due to equations non-linearity. An investigation was made to determine what range of values of the thrust parameter could be utilized to obtain a valid appro...
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| Format: | Others |
| Language: | en_US |
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Virginia Polytechnic Institute
2017
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| Online Access: | http://hdl.handle.net/10919/74556 |