| 摘要: |
| 提出了航空发动机数控系统三种抗积分器饱和算法。工程应用结果表明,三种算法均能有效抑止积分器饱和,提高了发动机数控系统的工作品质。算法实施简单,物理概念清楚,工程实用性强。 |
| 关键词: 航空发动机 数字控制器 控制系统 抗积分器饱和 |
| DOI： |
| 分类号:V233.7 |
| 基金项目:航空科学基金资助项目(04C14001) |
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| Investigation of integrator wind-up protection algorithms in aeroengine digital control system |
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JIANG Ping-guo,SUN Jian-guo
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1.Coll.of Energy and power,Nanjing Univ.of Aeronautics and Astronautics,Nanjing 210016,China;2.China Aviation Motor Control Inst.,Wuxi 214063,China
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| Abstract: |
| Three kinds of integrator wind-up protection(IWP) algorithms are proposed for aeroengine digital control system.The engineering applications show that each kind of algorithms can effectively restrain the integrator saturation and improve transient performance of aeroengine digital control system. |
| Key words: Aircraft engine Digital controller Control system Integrator wind-up protection |
