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原文请求
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题 名：
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Capability Description for NASA's F/A-18 TN 853 as a Testbed for the Integrated Resilient Aircraft Control Project
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并列题名：
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作 者：
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Hanson, C.
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作者机构：
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NASA Dryden Flight Research Center
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团体作者：
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摘 要：
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The NASA F/A-18 tail number (TN) 853 full-scale Integrated Resilient Aircraft Control (IRAC) testbed has been designed with a full array of capabilities in support of the Aviation Safety Program. Highlights of the system's capabilities include: 1) a quad-redundant research flight control system for safely interfacing controls experiments to the aircraft's control surfaces; 2) a dual-redundant airborne research test system for hosting multi-disciplinary state-of-the-art adaptive control experiments; 3) a robust reversionary configuration for recovery from unusual attitudes and configurations; 4) significant research instrumentation, particularly in the area of static loads; 5) extensive facilities for experiment simulation, data logging, real-time monitoring and post-flight analysis capabilities; and 6) significant growth capability in terms of interfaces and processing power.
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分 类 号：
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关 键 词：
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F-18 aircraft ;Aircraft control ;Flight control ;Static loads ;Real time operation ;Flight safety ;Adaptive control ;Aircraft safety ;Simulation ;Postflight analysis
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出 版 年：
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报 告 号：
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DFRC-IRAC-CAP-002; DFRC-972
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ISBN：
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NULL
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ISSN：
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NULL
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页 码：
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p.1-17
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页 数：
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17
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语 种：
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eng
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馆 藏 号：
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NTIS-N20090022324
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