直升机驱动控制仿真系统的设计与实现

2020 IEEE 15th International Conference on Nano/Micro Engineered and Molecular System (NEMS) Pub Date : 2020-09-27 DOI:10.1109/NEMS50311.2020.9265598

Zhigang Wu, Fuzheng Chen, Kaiming Xu, Xianmin Peng, U. Wejinya, G. Shi

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引用次数: 0

摘要

针对直升机试验的需要，设计并实现了直升机驱动控制仿真系统。本文介绍了该系统的硬件结构和工作原理、控制程序、空载和有载转速精度测试。根据实际应用和实验结果，通过现场试验验证了硬件和软件系统的可行性和有效性，直升机驱动控制系统的设计和实现很好地满足了直升机试验的要求。

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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Design and Implementation of Helicopter Drive Control Simulation System

For the demand of helicopter test, a helicopter drive control simulation system was designed and implemented. This paper describes the structure and principles of hardware, the control program, the non-load and load speed accuracy testing. According to the practical application and the experimental results, the feasibility and effectiveness of the hardware and software system are verified by field test, and the design and implementation of helicopter drive control system meets the requirements of helicopter test very well.

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来源期刊

2020 IEEE 15th International Conference on Nano/Micro Engineered and Molecular System (NEMS)

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