| 基于惯性导航的自动云台控制系统 |
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| 引用本文： | 叶祥,曹邦兴,李英杰.基于惯性导航的自动云台控制系统[J].仲恺农业技术学院学报,2007,20(2):45-48. |
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| 作者姓名： | 叶祥 曹邦兴 李英杰 |
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| 作者单位： | 1. 仲恺农业技术学院,机电工程系,广东,广州,510225
2. 广州大学,松田学院,广东,广州,511370 |
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| 摘 要： | 无人飞机上的摄像头拍摄地面固定对象时,需要根据无人飞机位置姿态的改变来控制摄像机云台.利用惯性导航原理获取系统姿态信息,然后使数据通过ARM处理来控制云台稳定,模拟结果表明这种设计符合系统的要求.
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| 关 键 词： | 云台 惯性导航 陀螺仪 加速度计 |
| 文章编号： | 1006-0774（2007）02-0045-04 |
| 收稿时间： | 2006-12-20 |
| 修稿时间： | 2006-12-20 |
An automatic pan-fit control system based on inertial navigator |
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| YE Xiang,CAO Bang-xing,LI Ying-jie.An automatic pan-fit control system based on inertial navigator[J].Journal of Zhongkai Agrotechnical College,2007,20(2):45-48. |
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| Authors: | YE Xiang CAO Bang-xing LI Ying-jie |
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| Institution: | 1.Department of Mechanical and Electrical Engineering, Zhongkai University of Agriculture and Technology, Guangzhou 510225, Claim; 2. Sontan College, Guangzhou University, Guangzhou 511370, China |
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| Abstract: | When a vidicon placed on an aircraft was used to shoot a stabel object,it should be controlled by apan-fit along with the change of the aircraft position.The inertial navigation system was used to get the position stance of vidicon and the pan-fit was controlled by the embeded arm system.Simulalion result showed that this design was adaptable to the request of the system. |
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| Keywords: | pan-fit inertial navigation gyro accelerator |
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