| Attitude Controller Design on Variable Rolling Velocity Aerocraft Based on ATmega16 |
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| 作者姓名： | Shi Guoxing Su Zhong Li Qing Chen Yingshu |
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| 作者单位： | Shi，Guoxing Su，Zhong Li，Qing Chen，Yingshu(Beijing Institute of Machinery，Beijing 100101) (Beijing XingJian ChangKong Measurement &Control Technology Co. Ltd) |
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| 基金项目： | This item is sponsored by science and technologydevelopment project of Beijing education commit-teeNO: KM200510772012 |
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| 摘 要： | 1 Introduction Owing to the effect of crosswind, initial disturbance and the deviation of engine parameters.etc in the initial aviation, variable rolling velocity aerocraft will produce attitude angle deviation (AAD) in the ideal orientations. It must control the attitude of the aerocraft, accordingly, AAD of aerocraft can be amended.Angle stabilization control system is used for the attitude control of rolling aerocraft by this paper. This control system is generally located in the control…
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| 关 键 词： | 变滚转速率 飞行器 姿态控制器 |
| 文章编号： | 1008-0570(2006)07-2-0100-03 |
| 修稿时间： | 2005年11月13 |
Attitude Controller Design on Variable Rolling Velocity Aerocraft Based on ATmega16 |
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| Shi,Guoxing Su,Zhong Li,Qing Chen,Yingshu.Attitude Controller Design on Variable Rolling Velocity Aerocraft Based on ATmega16[J].Control & Automation,2006,22(20):100-106. |
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| Authors: | Shi Guoxing Su Zhong Li Qing Chen Yingshu |
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| Abstract: | |
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| Keywords: | Rolling Velocity Aerocraft Attitude Controller |
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