| タイトル | Requirement analysis of an intelligent, redundant, actuation system |
| 著者（英） | De Feo, P.; Shih, K. C. |
| 著者所属（英） | NASA Ames Research Center|Sparta Systems, Inc. |
| 発行日 | 1986-01-01 |
| 言語 | eng |
| 内容記述 | The reliability and fault tolerance requirements of integrated, critical, digital fly-by-wire control systems for advanced military and civil aircraft requires redundant, reconfigurable implementations of the actuation system. An effective way for controlling the actuators and implementing the required fault detection and reconfiguration strategies is by means of dedicated microprocessors. This paper describes a laboratory implementation of a flexible intelligent redundant actuation system capable of demonstrating the concept and analyzing a variety of configurations and technical issues. |
| NASA分類 | AIRCRAFT INSTRUMENTATION |
| レポートNO | 87A16766 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/381076 |
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