| 炮射无人机飞行姿态稳定控制系统设计 |
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| 引用本文： | 吴维,王华,史晓霞. 炮射无人机飞行姿态稳定控制系统设计[J]. 战术导弹技术, 2005, 0(5): 56-60 |
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| 作者姓名： | 吴维 王华 史晓霞 |
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| 作者单位： | 北京航空航天大学,北京100083 |
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| 摘 要： | 为解决炮射无人机在巡航阶段的飞行姿态稳定控制问题,在考虑炮射无人机静稳定的前提下,运用改进的比例反馈控制方法,对炮射无人机的纵向和侧向二维线性模型,进行了姿态稳定控制仿真.仿真计算结果表明,比例反馈控制方法对炮射无人机的姿态稳定控制过程实用而有效.
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| 关 键 词： | 炮射无人机 比例反馈控制 姿态稳定 |
| 文章编号： | 1009-1300(2005)05-0056-05 |
| 修稿时间： | 2004-10-27 |
Design on Flight Attitude Stability Control System of Gun-launched Unmanned Aerial Vehicle |
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| Wu Wei,Wang Hua,Shi Xiaoxia. Design on Flight Attitude Stability Control System of Gun-launched Unmanned Aerial Vehicle[J]. Tactical Missile Technology, 2005, 0(5): 56-60 |
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| Authors: | Wu Wei Wang Hua Shi Xiaoxia |
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| Abstract: | To design the flight attitude stability control loop of gun-launched unmanned aerial vehicle(UAV) with longitudinal and lateral directional 2D linear model established in terms of the static stability condition during the cruise,the improved proportional feedback control method is employed to achieve the require of the settling time and steady-state precision.The simulative calculation results show that the improved proportional feedback control method works effectively in the flight attitude stability control of gun-launched UAV. |
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| Keywords: | gun-launched unmanned aerial vehicle proportional feedback control attitude stability |
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