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SYSTEM AND METHOD FOR DESIGNING OPTIMIZATION ALGORITHM FOR DETERMINING INTEGRITY OF AIRCRAFT STRUCTURAL
SYSTEM AND METHOD FOR DESIGNING OPTIMIZATION ALGORITHM FOR DETERMINING INTEGRITY OF AIRCRAFT STRUCTURAL
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机译:用于设计用于确定飞机结构完整性的优化算法的系统和方法
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摘要
Disclosed are a system and method for designing an optimization algorithm for judging the soundness of an aircraft structure. The present invention can design and provide an optimized algorithm capable of determining the structural integrity of an aircraft using flight tests and learning.
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