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火箭发动机燃烧过程无记忆鲁棒镇定的积分不等式方法
引用本文:李涛,张合新,孟飞.火箭发动机燃烧过程无记忆鲁棒镇定的积分不等式方法[J].宇航学报,2010,31(12).
作者姓名:李涛  张合新  孟飞
作者单位:第二炮兵工程学院自动化系,西安,710025
摘    要:研究了液体火箭发动机燃烧室燃烧过程的无记忆鲁棒镇定问题。通过构造适当的Lyapunov泛函并结合积分不等式变换技巧,将所得的非线性矩阵不等式转化为可解的线性矩阵不等式,导出了不确定时滞系统可鲁棒镇定的时滞相关条件。与现有方法相比,该方法不涉及模型变换技术,因而减少了理论与计算上的复杂性。同时在较大的参数变化范围内保证了燃烧过程的鲁棒镇定。最后通过数值仿真验证了其有效性。

关 键 词:火箭发动机  燃烧  鲁棒镇定  线性矩阵不等式  积分不等式  

Integral Inequality Approach to Memoryless Robust Stabilization of Combustion Process in Rocket Motor
LI Tao,ZHANG He-xin,MENG Fei.Integral Inequality Approach to Memoryless Robust Stabilization of Combustion Process in Rocket Motor[J].Journal of Astronautics,2010,31(12).
Authors:LI Tao  ZHANG He-xin  MENG Fei
Institution:LI Tao,ZHANG He-xin,MENG Fei(Department of Automation,Second Artillery Engineering College,Xi'an 710025,China)
Abstract:The memoryless robust stabilization of the combustion process in liquid propellant rocket motor chambers is investigated in this paper.By constructing appropriate Lyapunov functional combined with a integral inequality transformation technique,nonlinear matrix inequalities are transformed into linear ones and delay-dependent conditions for robust stabilization of the uncertain system with discrete delay are derived.Compared with existing methods,the proposed approach doesn't involve the model transformation...
Keywords:Rocket motors  Combustion  Robust stabilization  Linear matrix inequality(LMI)  Integral inequality  
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