| タイトル | Fly-by-light flight control system technology development plan |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900005795 |
| 著者（英） | Norton, R. L.; Chakravarty, A.; Griffith, D. M.; Berwick, J. W.; Marston, S. E. |
| 著者所属（英） | Boeing Commercial Airplane Co. |
| 発行日 | 1990-01-01 |
| 言語 | eng |
| 内容記述 | The results of a four-month, phased effort to develop a Fly-by-Light Technology Development Plan are documented. The technical shortfalls for each phase were identified and a development plan to bridge the technical gap was developed. The production configuration was defined for a 757-type airplane, but it is suggested that the demonstration flight be conducted on the NASA Transport Systems Research Vehicle. The modifications required and verification and validation issues are delineated in this report. A detailed schedule for the phased introduction of fly-by-light system components has been generated. It is concluded that a fiber-optics program would contribute significantly toward developing the required state of readiness that will make a fly-by-light control system not only cost effective but reliable without mitigating the weight and high-energy radio frequency related benefits. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 90N15111
NASA-CR-181953
NAS 1.26:181953 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/139330 |
