AEROENGINE TEST AUTOMATION OF ADAPTIVE CONTROL WITH RESTRAINTS

Fan Ding; Li Runzhi

Chinese

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AEROENGINE TEST AUTOMATION OF ADAPTIVE CONTROL WITH RESTRAINTS

更新时间：2026-07-07

- AEROENGINE TEST AUTOMATION OF ADAPTIVE CONTROL WITH RESTRAINTS
- Vol. 12, Issue 4, (1997)
- 作者机构：
  
  1. 西北工业大学
  2. 南方动机机械公司
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：1997
- 稿件说明：
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Fan Ding, Li Runzhi. AEROENGINE TEST AUTOMATION OF ADAPTIVE CONTROL WITH RESTRAINTS[J]. 1997, 12(4).
DOI：

Fan Ding, Li Runzhi. AEROENGINE TEST AUTOMATION OF ADAPTIVE CONTROL WITH RESTRAINTS[J]. 1997, 12(4). DOI：

摘要

对采用模型参考自适应控制方法设计带有多项约束条件的航空发动机试车自动试车控制系统进行了研究。仿真结果表明：这种控制方法不仅对被控对象含有的非线性环节

以及被控对象参数在较大范围内的变化具有较好的适应能力。而且当约束条件超限时

通过对控制器参数的调整

可使主控参数和约束条件参数均满足相应的控制指标。

Abstract

An automatic control system of aeroengine test has been designed

based on the method of model reference adaptive control with restraints.According to its simulation results

this method has good adaptability when the controlled member contains non-linear elements or the controller member varies in a large range.The simulation results also show that

the controlled system still has satisfactory performance index by regulating the controller's parameters

even if the restraints are out of limits.

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