| 无人直升机飞控系统设计与应用 |
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| 引用本文： | 顾冬雷,夏先明,高正.无人直升机飞控系统设计与应用[J].南京航空航天大学学报,2005,37(4):476-478. |
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| 作者姓名： | 顾冬雷 夏先明 高正 |
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| 作者单位： | 南京航空航天大学直升机旋翼动力学国家重点实验室,南京,210016;南京模拟技术研究所,南京,210016 |
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| 摘 要： | 论述了将Voyage模型直升机改造成全自主无人直升机的工作。首先，改造了直升机结构，设计了飞控电子设备和基于客户／服务模式的飞控软件和地面站软件；其次，利用扫频数据进行频域辨识，建立了直升机姿态通道的动力学模型；最后，设计了飞行控制律，实现了在悬停和低速下的全自主飞行。
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| 关 键 词： | 无人直升机 电子设备 频域辨识 飞行控制 |
| 文章编号： | 1005-2615(2005)04-0476-03 |
| 收稿时间： | 2004-12-15 |
| 修稿时间： | 2004年12月15 |
Design of Flying Control System for an Autonomous Helicopter |
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| GU Dong-lei,XIA Xian-ming,GAO Zheng.Design of Flying Control System for an Autonomous Helicopter[J].Journal of Nanjing University of Aeronautics & Astronautics,2005,37(4):476-478. |
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| Authors: | GU Dong-lei XIA Xian-ming GAO Zheng |
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| Abstract: | The Voyage model helicopter is changed into a full autonomous helicopter. The main contributions include the design of avionics system based on PC104, the software design based on the client/server architecture, and the modeling of helicopter dynamics based on the frequency sweep and frequency domain identification. The flying control laws are implemented, thus realizing the helicopter autonomous flying under hover and low speed conditions. |
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| Keywords: | autonomous helicopter avionics system frequency domain identification flying control |
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