| 带积分项的火箭炮最优化滑模伺服控制 |
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| 引用本文： | 朱玉川,马大为,李志刚,乐贵高.带积分项的火箭炮最优化滑模伺服控制[J].兵工学报,2007,28(10):1272-1275. |
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| 作者姓名： | 朱玉川 马大为 李志刚 乐贵高 |
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| 作者单位： | 1．南京航空航天大学机电学院，江苏南京210016；2．南京理工大学机械工程学院，江苏南京210094 |
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| 摘 要： | 针对某防空火箭炮交流位置伺服系统负载、参数大范围变化以及发射时具有强干扰力矩的特点，提出了带积分项的基于最优化的滑模变结构控制方法并设计了控制器。计算机仿真结果表明，该控制器不仅消除了经典控制所存在的静差，同时对负载扰动和系统参数摄动具有较强的鲁棒性，并保证了系统的瞬态性能指标。
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| 关 键 词： | 自动控制技术 兵器发射理论与技术 火箭炮 滑模变结构控制 切换函数 控制律 |
| 文章编号： | t000-1093（2007）10-1272-04 |
| 修稿时间： | 2005-12-26 |
Optimal Sliding Mode Servo Control with Integral Term for Rocket Launcher |
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| ZHU Yu-chuan,MA Da-wei,LI Zhi-gang,LE Gui-gao.Optimal Sliding Mode Servo Control with Integral Term for Rocket Launcher[J].Acta Armamentarii,2007,28(10):1272-1275. |
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| Authors: | ZHU Yu-chuan MA Da-wei LI Zhi-gang LE Gui-gao |
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| Affiliation: | 1.College of Mechanical and Electrical Engineering, Nanjing Limversity of Aeronautics and Astronautics,
Nanjing 210016, Jiangsu, China; 2. School of Mechanical Engineering, Nanjing Ijmversity of Science and Technology, Nanjing 210094，Jiangsu, China |
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| Abstract: | An AC position servo system of air defense rocket launcher was designed. Based on wide variations in loads and parameters and large disturbed moment, an optimal sliding mode variable struc- ture servo control method with integral term was presented, and a controller was designed. The com- puter simulation results show that steady state error which is present at classical control is eliminated, the system takes on strong robustness to load disturbance and parameter perturbation, and ensures, transient state performance figure of the system. |
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| Keywords: | automatic control technology armament launch theory and technology rocket launchersliding mode variable structure control switching function control law |
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