| 基于Ackermann规则的离散全程灰色滑模控制在数字导弹姿态控制系统中的应用 |
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| 引用本文： | 米文鹏,闫双卡,杨建飞,洪成华. 基于Ackermann规则的离散全程灰色滑模控制在数字导弹姿态控制系统中的应用[J]. 电光与控制, 2009, 16(4) |
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| 作者姓名： | 米文鹏 闫双卡 杨建飞 洪成华 |
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| 作者单位： | 第二炮兵工程学院,西安,710025;第二炮兵青州士官学校,山东,青州,262500 |
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| 摘 要： | 针对数字式导弹姿态控制系统的参数具有时变性和不确定性的特点,设计了一种离散变结构控制器.该控制器结合了Ackermann规则设计切换函数简单、易行的优点和全程滑模控制器的全局鲁棒性的长处.同时引入灰色理论,设计了灰色补偿控制项,用于克服数字导弹姿态控制系统的不确定项对系统造成的影响.结果表明,该控制器在导弹姿态控制系统中的仿真效果较为令人满意.
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| 关 键 词： | 导弹姿态控制 Ackermann规则 全程滑态变结构控制 姿态控制系统 全程滑态因子 灰色补偿控制项 |
Application of Ackermann Formula Based Discrete Grey Sliding Mode Control in Digital Missile Attitude Control System |
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| MI Wenpeng,YAN Shuangka,YANG Jianfei,HONG Chenghua. Application of Ackermann Formula Based Discrete Grey Sliding Mode Control in Digital Missile Attitude Control System[J]. Electronics Optics & Control, 2009, 16(4) |
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| Authors: | MI Wenpeng YAN Shuangka YANG Jianfei HONG Chenghua |
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| Affiliation: | 1.The Second Artillery Engineering College;Xi'an 710025;China;2.The Second Artillery Qingzhou Petty Officer School;Qingzhou 262500;China |
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| Abstract: | The parameters of digital missile attitude-control system are time-varying and uncertain,thus we designed a discrete Variable Sliding Controller(VSC).The design combined the advantages of Ackermann's formula that the sliding function is simple and easily implemented,and advantage of the global VSC of the global robustness.Grey theory was introduced for designing a grey compensator to eliminate the bad influence of uncertainty.The result showed that the controller had satisfactory effect when using in simula... |
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| Keywords: | missile attitude control Ackermann's formula global VSC attitude control system global sliding gene grey compensatory controller |
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