| 小型无人机自主飞行控制系统的实现 |
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| 引用本文： | 陈天华,郭培源.小型无人机自主飞行控制系统的实现[J].航天控制,2006,24(5):86-90. |
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| 作者姓名： | 陈天华 郭培源 |
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| 作者单位： | 北京工商大学信息工程学院,北京,100037 |
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| 摘 要： | 介绍了5kg级小型无人机的结构原理,分析了无人机自主飞行控制系统的结构、功能、特点及控制原理,采用嵌入式系统、GPS、电子罗盘和红外传感器等设计了无人机的飞行姿态控制、导航控制、任务控制系统和弹射与伞降系统。大量飞行实践和比赛飞行表明,这种小型无人机可执行既定任务并具有良好的场地适应性和自主飞行性能。
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| 关 键 词： | 无人机 自主飞行 空中机器人 飞行控制 |
| 文章编号： | 1006-3242(2006)05-0086-05 |
| 修稿时间： | 2006年4月11日 |
Realization of Autonomous Flight Control System of Mini-unmaned Aerial Vehicles |
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| Chen Tianhua,Guo Peiyuan.Realization of Autonomous Flight Control System of Mini-unmaned Aerial Vehicles[J].Aerospace Control,2006,24(5):86-90. |
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| Authors: | Chen Tianhua Guo Peiyuan |
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| Abstract: | The architecture and principle of 5kg UAV is introduced,and the structure,function,characteristic and the principle of control system of UAV are analyzed.The flight attitude control,navigation control,mission control system,launch system and landing system are designed by using embedded-microcomputer system,GPS,electronic compass and infrared sensor.The flight experiments and flight competitions show that the UAV can perform a mission prescribed in advance.It has good adaptability for circumstance and can fly autonomously. |
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| Keywords: | Unmaned aerial vehicles Autonomous flight Aerial robotics Flight control |
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