摘要
Helicopter mathematical model mainly depends on design helicopter control system, flight simulator, and real time control simulation system. But it is difficult to establish a helicopter flight dynamics mathematical model that has features such as rapidness, reliability and precision, because there is no unique and precise expression to some sophisticated phenomenon of helicopter. In this paper a fuzzy helicopter flight model is constructed based on the flight experimental data. The fuzzy model, which is identified by fuzzy inference, has characteristics of computed rapidness and high precision. In order to guarantee the precision of the identified fuzzy model, a new method is adopted to handle the conflict fuzzy rules. Additionally, using fuzzy clustering technology can effectively reduce the number of rules of fuzzy model, namely, the order of the fuzzy model. The simulation results indicate that the method of this paper is effective and feasible.
直升机控制系统的设计、飞行模拟器的研制及计算机实时仿真都离不开直升机数学模型 ,但是建立可靠而且准确的直升机飞行动力学模型是十分困难的 ,而且也很难保证动力学模型计算的快速性、可靠性与实时性。本文基于模糊推理技术 ,根据飞行试验数据辨识了直升机飞行模型 ,可以在一定程度上保证所辨识模型的简单、准确与计算的实时性。为了提高模糊模型的精度 ,文中采用了一种新方法来处理矛盾规则。本文利用模糊聚类分析的方法对海量的试验样本数据进行处理 ,有效地减少了辨识模型的规则数量。最后的仿真辨识结果表明 ,辨识效果合理 ,方法可行。
