| 采用智能阻尼的飞航导弹过载控制 |
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| 引用本文： | 王宏然,程继红,张友安.采用智能阻尼的飞航导弹过载控制[J].海军航空工程学院学报,2006,21(2):231-233. |
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| 作者姓名： | 王宏然 程继红 张友安 |
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| 作者单位： | 1. 海军航空工程学院控制工程系
2. 海军航空工程学院科研部,山东,烟台,264001 |
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| 基金项目： | 解放军总装备部预研重点基金 |
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| 摘 要： | 首先分析了经典的飞航导弹过载控制系统结构,指出了其不足之处。然后给出了一种简单有效的基于规则的智能阻尼过载控制方法。同时,在控制设计过程中通过引入角加速度反馈相当于考虑了舵机的动态特性,使控制系统的动态性能得到进一步改善。最后,仿真结果验证了该方法的正确性和有效性。
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| 关 键 词： | 飞航导弹 导弹过载控制 智能控制 智能阻尼 |
| 修稿时间： | 2005年10月28 |
Overload control for winged missile using intelligent resistance |
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| WANG Hongran,CHENG Jihong and ZHANG You''an.Overload control for winged missile using intelligent resistance[J].Journal of Naval Aeronautical Engineering Institute,2006,21(2):231-233. |
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| Authors: | WANG Hongran CHENG Jihong and ZHANG You'an |
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| Institution: | Department of Control Engineering,NAEI,Department of Scientific Research,NAEI,Yantai,Shandong,264001 and Department of Control Engineering,NAEI |
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| Abstract: | First, classical overload control system structures for winged missile are analyzed, and their shortages are pointed out. Then, a simple effective overload control method for winged missile using intelligent resistance is presented. Simultaneously, the dynamics of the actuator are taking into account in the control system design process by introducing angular rate feedback, and thus the performance of the control system in transient response are further improved. Finally, simulation results show that the proposed method is right and effective. |
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| Keywords: | winged missile overload control for missile intelligent control intelligent resistance |
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