The Engineering Analysis and Design of the Aircraft Dynamics Model For the FAA Target Generation Facility
The derivation of the six degree of freedom equations of motion. The Earth model, its kinematic parameters. An analytical solution in the discrete time interval. Choosing a single reference condition for gain calculation. Aircraft device deployment.
| Рубрика | Транспорт |
| Вид | учебное пособие |
| Язык | английский |
| Дата добавления | 02.07.2014 |
| Размер файла | 3,7 M |
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