| 摘要: |
| 以成功设计的航空发动机液压机械控制系统和模拟电子控制系统为基础,从中抽取出了相应的控制逻辑,并将它们应用到了数字电子控制系统设计当中。仿真表明,控制逻辑设计的应用是成功的,它可以大大简化控制系统结构,为鲁棒控制器等高阶控制器在航空发动机数字电子控制系统中的应用奠定了基础。 |
| 关键词: 航空发动机 控制 控制仿真 逻辑设计 |
| DOI： |
| 分类号:V233.7 |
| 基金项目: |
|
| Aeroengine control logic design |
|
ZHENG Tie-jun,WANG Xi,LUO Xiu-qin,LI Qi-han
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1.Coll.of Energy and Power Engineering,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;2.Engineering Inst.,Air Force Engineering Univ.,Xi’an 710038,China
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| Abstract: |
| The control logic is abstracted from some successfully designed aeroengine hydraulic machinery control systems and analog electronic control systems and it is applied to the design of the numerical control system of a certain aeroengine.Simulation shows that the application of the control logic is successful.The construction of the control system is greatly simplified. |
| Key words: Aircraft engine Control Control simulation,Logic design |
