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本文提出一种实用的以刚度设计为主的直升机硬式操纵系统设计方法,运用结构优化理论和敏度分析技术,对系统自身结构和系统机体支持结构分别进行刚度和强度设计。
In this paper, a practical design method of helicopter rigid control system based on stiffness design is proposed. Using the theory of structure optimization and the sensitivity analysis, the stiffness and strength of the system itself and the system support structure are designed respectively.