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基于模糊建模的非线性鲁棒模型预测控制 被引量:2
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作者 刘志远 周建锁 +1 位作者 裴润 陈虹 《电机与控制学报》 EI CSCD 北大核心 2002年第3期229-232,236,共5页
针对离散不确定模糊模型,提出了一种鲁棒非线性模型预测控制方法。导出了预测性能指标上界,将稳定性约束、输入约束和输出约束变换成容易求解的线性矩阵不等式(LMI)形式,从而将非线性模型预测控制Min-Max优化问题变换成具有线性矩阵... 针对离散不确定模糊模型,提出了一种鲁棒非线性模型预测控制方法。导出了预测性能指标上界,将稳定性约束、输入约束和输出约束变换成容易求解的线性矩阵不等式(LMI)形式,从而将非线性模型预测控制Min-Max优化问题变换成具有线性矩阵不等式约束的广义特征值问题(GEVP)。对于采用的状态反馈预测控制器,讨论了滚动时域优化的可行性,证明了闭环系统的鲁棒稳定性。仿真结果表明了控制器的有效性。 展开更多
关键词 模糊建模 非线性鲁棒模型 预测控制 线性矩阵不等式
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Nonlinear Rolling Control Technology of Liquid Launch Vehicle Based on Single Engine
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作者 ZHANG Weidong DING Xiufeng +1 位作者 LIU Yuxi XUE Yu 《Aerospace China》 2016年第1期12-18,共7页
New program was proposed in LM-6 rolling control technology that using high-pressure staged combustion gas. Launch vehicle rolling control by just one engine was realized. Under the limit of the rolling control moment... New program was proposed in LM-6 rolling control technology that using high-pressure staged combustion gas. Launch vehicle rolling control by just one engine was realized. Under the limit of the rolling control moment of the launch vehicle, a new attitude dynamic model is established. Interference source and how to reduce the effect was analyzed, and method of designing a pre-compensated robust controller was proposed. Simulation and flight resuits showed that the attitude dynamic model established and the pre-compensation robust controller proposed in this paper could solve the key problems with a strong coupling attitude controller, and realize high quality and high reliability control in wind areas, and improve the capability of the launch vehicle. 展开更多
关键词 LM-6 Rolling control Attitude model Attitude control.
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