大型直升机模型及其验证

A. Gee, T. Clarke, P. Taylor
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引用次数: 2

摘要

在任何工作领域使用建模和模拟都必须通过了解这些模型的有效程度来调节。建模缺陷和近似导致准确性丧失的条件必须明确界定,以便使用此类模型的研究或实验调查产生有意义的结果。本文考虑对EH-101直升机进行大规模非线性仿真验证,并将模型性能与实际飞行数据进行比较。描述了模型的结构和实现,以及提出的验证技术、导频建模函数和调优方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A large-scale helicopter model and its validation
The use of modelling and simulation in any sphere of work must be tempered by an understanding of the extent to which such models are valid. The conditions under which modelling deficiencies and approximations cause accuracy to be lost must be clearly defined so that research or experimental investigations using such models yield meaningful results. This paper considers the validation of a large-scale nonlinear simulation of the EH-101 helicopter, comparing the performance of the model with actual flight data, taken from the real helicopter. The structure and implementation of the model are described together with the proposed validation technique, pilot modelling functions and tuning approaches.
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