| タイトル | Advanced piloted aircraft flight control system design methodology. Volume 1: Knowledge base |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890016642 |
| 著者（英） | Myers, Thomas T.; Mcruer, Duane T. |
| 著者所属（英） | Systems Technology, Inc. |
| 発行日 | 1988-10-01 |
| 言語 | eng |
| 内容記述 | The development of a comprehensive and electric methodology for conceptual and preliminary design of flight control systems is presented and illustrated. The methodology is focused on the design stages starting with the layout of system requirements and ending when some viable competing system architectures (feedback control structures) are defined. The approach is centered on the human pilot and the aircraft as both the sources of, and the keys to the solution of, many flight control problems. The methodology relies heavily on computational procedures which are highly interactive with the design engineer. To maximize effectiveness, these techniques, as selected and modified to be used together in the methodology, form a cadre of computational tools specifically tailored for integrated flight control system preliminary design purposes. While theory and associated computational means are an important aspect of the design methodology, the lore, knowledge and experience elements, which guide and govern applications are critical features. This material is presented as summary tables, outlines, recipes, empirical data, lists, etc., which encapsulate a great deal of expert knowledge. Much of this is presented in topical knowledge summaries which are attached as Supplements. The composite of the supplements and the main body elements constitutes a first cut at a a Mark 1 Knowledge Base for manned-aircraft flight control. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 89N26013
STI-TR-1228-1
NASA-CR-181726-VOL-1
NAS 1.26:181726-VOL-1 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/141382 |
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