| 微小型无人机全姿态增稳控制系统的设计与实现 |
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| 引用本文： | 迟晓鹏,罗卫兵,霍丽霞.微小型无人机全姿态增稳控制系统的设计与实现[J].现代电子技术,2010,33(8):160-162. |
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| 作者姓名： | 迟晓鹏 罗卫兵 霍丽霞 |
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| 作者单位： | 武警工程学院,陕西,西安,710086 |
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| 基金项目： | 国家反恐"709"计划--武警部队重点科研项目 |
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| 摘 要： | 针对传统微小型无人机在飞行过程中存在的稳定性问题,指出影响稳定的因素。提出一种基于三轴陀螺和倾角传感器构成全姿态增稳控制系统的设计方案,采用EWTS82三轴陀螺和SCA100T双轴传感器组成姿态增稳硬件控制,结合软件增稳控制,成功应用到某型微小型无人机上。大量的试飞结果表明,基于三轴陀螺和倾角传感器构成的姿态增稳控制系统优于传统的测量单元,有很好的应用价值。
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| 关 键 词： | 无人机 三轴陀螺 倾角传感器 增稳控制 |
Design and Implementation of All-attitude Stability Augmentation Control System of Miniature UAV |
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| CHI Xiao-peng,LUO Wei-bing,HUO Li-xia.Design and Implementation of All-attitude Stability Augmentation Control System of Miniature UAV[J].Modern Electronic Technique,2010,33(8):160-162. |
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| Authors: | CHI Xiao-peng LUO Wei-bing HUO Li-xia |
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| Affiliation: | CHI Xiao-peng,LUO Wei-bing,HUO Li-xia (Engineering College of Armed Police Force,Xi\'an 710086,China) |
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| Abstract: | According to the problems existing in flight process of traditional miniature UAV,the factors that affects the stability is pointed out,and a design scheme of all-attitude stability augmentation control system based on the tri-axis gyroscrope and tilt angle sensor is proposed.The hardware control system of attitude stability augmentation is comprised of EWTS82 tri-axis gvroscrope and SCA100T dual-axis sensor.It was applied to a certain type of miniature UAV successfully in combination with a software of sta... |
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| Keywords: | UAV tri-axis gyro tilt angle sensor all-attitude stalility augmentation control |
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