Accurate mathematical model for describing electrohydraulic loading system of helicopter pitch adjusting hydromechanical servos

Guojian Liu, Yunhua Li, Liman Yang
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引用次数: 3

Abstract

This paper deals with the establishment of the exact mathematical model for describing the electro-hydraulic load system which is applied to the earth-experiment of the hydromechanical servomechanism (hydraulic assistor) for the helicopter pitch adjusting. Based on the working principle analysis of the electro-hydraulic load system, the accurate mathematical model of electric-hydraulic loading system is established and the influence of the model on the system characteristics is deeply analyzed. It is proved that surplus force is concerned with not only the velocity but also the acceleration of rudderpost. Moreover, the traditional structure invariance principle is improved. Experiments in the paper validate the correctness of complex mathematical model, of which the guiding effect in eliminating the extraneous force is revealed also.
描述直升机俯仰调节液压伺服系统电液加载系统的精确数学模型
建立了用于直升机调纵液压伺服机构(液压助力器)地面试验的电液负载系统的精确数学模型。在分析电液加载系统工作原理的基础上,建立了电液加载系统的精确数学模型,并深入分析了该模型对系统特性的影响。证明了剩余力不仅与速度有关,而且与舵柱加速度有关。同时,对传统的结构不变性原理进行了改进。本文的实验验证了复杂数学模型的正确性,并揭示了该模型对消除外加力的指导作用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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