航模直升机飞行控制系统的设计与实现 |
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引用本文: | 刘培强,曾国贵,黄海,沈建平,祖家奎.航模直升机飞行控制系统的设计与实现[J].直升机技术,2009(4). |
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作者姓名: | 刘培强 曾国贵 黄海 沈建平 祖家奎 |
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作者单位: | 1. 南京航空航天大学,南京,210016 2. 中国直升机设计研究所,景德镇,333001 3. 元锡汉和航空技术有限公司,无锡,221000 |
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摘 要: | 针对40Kg级的航模直升机的技术特点,构建了飞行控制系统的硬件架构,研制出来了基于DSP和ARM双CPU系统的飞控计算机;详细介绍了基于μC/OS-Ⅱ实时操作系统的DSP/ARM双系统的机载飞控软件架构和功能模块;最后,鉴于直升机控制的技术难度和航模直升机特殊的飞行特点,对航模直升机的控制思想、控制策略以及飞行试验提出了自己的认识和实施路线。
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关 键 词: | 航模直升机 飞行控制 硬件设计 软件设计 控制律 |
Design of Flight Control System for Great Aero-Model Helicopter |
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Authors: | LIU Peiqiang ZENG Guogni HUANG Hai SHENG Jianping ZU Jiakui |
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Institution: | 1(1.College of Automation Engineering; Nanjing University of Aeronautics and Astronautics; Nanjing; 210016; 2.China Helicopter Research and Development Institute; Jingdezhen; 333001; 3.Hanhe Aero-Technique Inc; Wuxi; 221000); |
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Abstract: | Aimed at the characteristic technology of great aero-model helicopter about 40kg,It has constructed a hardware structure of flight control system and manufactured a flight control computer based on a double CPU system using DSP and ARM.Introduced the details of the structure and function module of the flight control software of the DSP/ARM double CPU system based on μC/OS-Ⅱ real-time operation system.In the end,it describes my own understanding of the control idea and tactic of helicopter and the course of ... |
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Keywords: | aero-model helicopter flight control hardware design software design control law |
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