| タイトル | High-speed civil transport flight- and propulsion-control technological issues |
| 本文（外部サイト） | http://hdl.handle.net/2060/19920012010 |
| 著者（英） | Carlin, C. M.; Ray, J. K.; Lambregts, A. A. |
| 著者所属（英） | Boeing Commercial Airplane Co.|PRC Kentron, Inc.|NASA Hugh L. Dryden Flight Research Facility |
| 発行日 | 1992-03-01 |
| 言語 | eng |
| 内容記述 | Technology advances required in the flight and propulsion control system disciplines to develop a high speed civil transport (HSCT) are identified. The mission and requirements of the transport and major flight and propulsion control technology issues are discussed. Each issue is ranked and, for each issue, a plan for technology readiness is given. Certain features are unique and dominate control system design. These features include the high temperature environment, large flexible aircraft, control-configured empennage, minimizing control margins, and high availability and excellent maintainability. The failure to resolve most high-priority issues can prevent the transport from achieving its goals. The flow-time for hardware may require stimulus, since market forces may be insufficient to ensure timely production. Flight and propulsion control technology will contribute to takeoff gross weight reduction. Similar technology advances are necessary also to ensure flight safety for the transport. The certification basis of the HSCT must be negotiated between airplane manufacturers and government regulators. Efficient, quality design of the transport will require an integrated set of design tools that support the entire engineering design team. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 92N21253
NAS 1.26:186015
H-1794
NASA-CR-186015 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/128300 |
