| 建立航空发动机状态空间模型的修正方法 |
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| 引用本文： | 郑铁军,王曦,罗秀芹,李其汉.建立航空发动机状态空间模型的修正方法[J].推进技术,2005,26(1):46-49. |
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| 作者姓名： | 郑铁军 王曦 罗秀芹 李其汉 |
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| 作者单位： | 1. 北京航空航天大学,能源与动力工程学院,北京,100083
2. 空军工程大学,工程学院,陕西,西安,710038 |
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| 摘 要： | 以阶跃输入响应进行模型的检验，提出了状态空间模型的修正方法：基于动态响应较好的状态空间模型，进行其矩阵B，D，F，G的修正，获得基于稳态修正的模型，解决了航空发动机状态空间模型检验与修正的问题。仿真表明，使用该方法修正的状态空间模型具有与原非线性数学模型完全一致的稳态响应和基本一致的动态过程响应。这种方法为航空发动机多变量数字电子控制器的设计奠定了强有力的基础。
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| 关 键 词： | 航空发动机 控制 状态空间模型 检验 仿真 |
| 文章编号： | 1001-4055(2005)01-0046-04 |
| 修稿时间： | 2004年3月22日 |
Modified method of establishing the state space model of aeroengine |
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| ZHENG Tie-jun,WANG Xi,LUO Xiu-qin and LI Qi-han.Modified method of establishing the state space model of aeroengine[J].Journal of Propulsion Technology,2005,26(1):46-49. |
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| Authors: | ZHENG Tie-jun WANG Xi LUO Xiu-qin and LI Qi-han |
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| Institution: | ZHENG Tie-jun~1,WANG Xi~1,LUO Xiu-qin~2,LI Qi-han~1 |
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| Abstract: | The verification and modification problems of the state space model of aeroengine is concerned. The model of interest is verified based on its step response and a kind of modification method to the model is provided: the model which has abetter dynamic response is selected and its matrix B, D, F, G is modified based on its steady response. Simulation demonstrates that this method can achieve a desirable steady state output and an almost exact dynamical behavior as the original nonlinear model. The proposed method can be applied to the establishment of the aeroengine state space model, which will be helpful in the multivariable digital electronic engine control system design. |
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| Keywords: | Aircraft engine Control State space model Inspection Eimulation |
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