C-17-flight-control-system-review
于 2011-05-02 发布
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代码说明：
：文章从满足C 17设计基本要求人手，阐述了避免严重失速的机理、操纵失效概率、所有发动机停车操 纵以及安全复飞要求。对综合飞行控制系统设计做了介绍。对满足上述要求的FCS特性做了描述。最后对早期的飞行试验结果作了分析。(: Articles from the design to meet the basic requirements of C 17 staff, described the mechanism to avoid serious stall, control failure probability, all the engines go around parking control and security requirements. The integrated flight control system design is introduced. FCS on the properties meet the above requirements was described. Finally, the early flight test results are analyzed.)
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