火力与指挥控制Issue(2)：108-112,5.
改进幂指数趋近律的航空发动机模糊滑模控制
Fuzzy Sliding Mode Controller For Aeroengine Based on An Improved Power Exponential Reaching Law
田虎森 1谢寿生 1苗卓广 1王磊 2任立通1
作者信息
- 1. 空军工程大学航空航天工程学院，西安 710038
- 2. 解放军95961部队，北京 100195
- 折叠
摘要
Abstract
For the reaching process of sliding mode variable structure control without robustness,a method of fuzzy sliding mode controller for aeroengine based on an improved power exponential reaching law is put forward. The sliding mode surface adapted automatically by fuzzy system is proposed,which can shorten the time of reaching process to enhance the robustness by making the sliding mode surface near the system state. And an improved power exponential reaching law is designed,weakens the chattering. Simulation results show that the devised controller has good effect, effectively restrains the influence and weakens the chattering.关键词
航空发动机/鲁棒性/滑模变结构控制/趋近律/抖振Key words
aero-engine/robustness/sliding mode variable structure control/reaching law/chattering分类
航空航天引用本文复制引用
田虎森,谢寿生,苗卓广,王磊,任立通..改进幂指数趋近律的航空发动机模糊滑模控制[J].火力与指挥控制,2016,(2):108-112,5.
