| 无人机自动空中加油精确对接控制 |
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| 引用本文： | 王宏伦,杜熠,盖文东.无人机自动空中加油精确对接控制[J].北京航空航天大学学报,2011,37(7):822-826. |
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| 作者姓名： | 王宏伦 杜熠 盖文东 |
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| 作者单位： | 北京航空航天大学飞行器控制一体化技术重点实验室,北京,100191;北京航空航天大学飞行器控制一体化技术重点实验室,北京,100191;北京航空航天大学飞行器控制一体化技术重点实验室,北京,100191 |
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| 基金项目： | 中央高校基本科研业务费专项资金资助项目(YWF-10-01-B015) |
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| 摘 要： | 针对无人机自动空中加油对接段的精确控制问题,提出了无人机自动空中加油的控制方案和策略,并在分析加油机尾涡干扰和加油锥套自由摆动及其对受油机影响的基础上,设计了适用于自动空中加油精确对接控制的受油机参考轨迹发生器和轨迹跟踪控制器.轨迹跟踪控制器采用线性二次型调节器方法,并充分考虑了加油过程中各种干扰的影响.仿真结果表明,该导引控制方法具有良好的快速性和抗干扰能力,可以满足空中加油的任务要求.
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| 关 键 词： | 无人机 自动空中加油 轨迹跟踪 线性二次型调节器 |
| 收稿时间： | 2010-08-10 |
Precise docking control in unmanned aircraft vehicle automated aerial refueling |
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| Wang Honglun Du Yi Gai Wendong.Precise docking control in unmanned aircraft vehicle automated aerial refueling[J].Journal of Beijing University of Aeronautics and Astronautics,2011,37(7):822-826. |
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| Authors: | Wang Honglun Du Yi Gai Wendong |
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| Institution: | Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics and Astronautics, Beijing 100191, China |
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| Abstract: | The control scheme and strategy for unmanned aircraft vehicle automated aerial refueling were proposed based on analysis of the vortex effect of tank and the free oscillation of drogue.The improved reference trajectory generator and trajectory tracking controller for receiver were used for automated aerial refueling precise docking control.The linear quadratic regulator method was used to design the trajectory tracking controller,and all kinds of disturbance were considered.The results of simulation show th... |
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| Keywords: | unmanned aircraft vehicle automated aerial refueling trajectory tracking linear quadratic regulator |
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