直升机悬停智能模糊飞行控制系统

M. Lower, B. Szlachetko, Dariusz Król
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引用次数: 18

摘要

本文研究了PZL卡尼亚单旋翼直升机现场悬停模糊飞行控制系统。在专家分析(飞行员知识)的基础上进行计算机仿真实验,建立了模糊控制系统的模型。利用Matlab软件包对直升机的数学模型和模糊飞控系统进行了仿真。在一系列的计算机模拟中,研究了模糊控制系统的运行情况,并对系统进行了调整。对直升机进行了固定悬停和有干扰悬停的仿真试验。扰动与一阵风或其中一个舵的偶然运动有关。所得结果为构建Web模拟器提供了良好的前景。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Fuzzy flight control system for helicopter intelligence in hover
This paper relates to a fuzzy flight control system in spot hovering for a single-rotor helicopter PZL Kania. The model of the fuzzy control system was developed on the basis of computer simulation experiments done by the expert's analysis (pilot's knowledge). The helicopter's mathematical model and its fuzzy flight control system were simulated using Matlab software package. In a series of numerous computer simulations the operation of the fuzzy control system was investigated and the system itself was tuned up. Simulation tests have been performed for the helicopter both in fixed hovering, and in hovering with disturbances. Disturbances were related to a gust of wind or to an accidental motion of one of the rudders. Obtained results give the good promise for building the Web simulator.
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