| タイトル | Generic multi-body formulation of heavy lift airship equations of motion |
| 著者（英） | Ringland, R. F.; Ashkenas, I. L.; Tischler, M. B.; Jex, H. R. |
| 著者所属（英） | Systems Technology, Inc. |
| 発行日 | 1980-01-01 |
| 言語 | eng |
| 内容記述 | This paper describes the formulation of a comprehensive set of equations which describe the dynamic behavior of a generic heavy lift airship (HLA). They are being used in a digital computer simulation to investigate the response dynamics and flying qualities of HLAs operating with various payloads in a variety of operational environments. A key feature is the separate treatment of each component body making up the HLA. This allows the analyst to vary the configuration (e.g., number of lift-propulsion units, presence or absence of slung payload, etc.) without rewriting the equations. It further provides measures of key structural and control loads acting on the HLA and eases the task of modeling wind disturbances. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 81A45539 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/415335 |
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