| Design for aircraft engine multi-objective controllers with switching characteristics | |
| Alternative Title | Design for aircraft engine multi-objective controllers with switching characteristics |
| Liu Xiaofeng1; Shi Jing1; Qi Yiwen2; Yuan Ye1 | |
| 2014 | |
| Source Publication | Chinese Journal of Aeronautics
 |
| ISSN | 1000-9361 |
| Volume | 27Issue:5Pages:1097-1110 |
| Abstract | The aircraft engine multi-loop control system is described and the switching control theory is introduced to solve the regulating and protecting control problems in this paper. The aircraft engine multi-loop control system is firstly described and the control problems are formulated. Secondly, the theory of the smooth switching control is devoted and a new extended scheme for the smooth switching of a switched control system is introduced. Then, for the key technologies of aero-engines switching control, a design algorithm is presented which can determine which candidate controller should be put in feedback with the plant to achieve a desired performance and the procedure to design the aircraft engine multi-loop control system is detailed. The switching performance objectives and the switching scheme are given and a family of PID controllers and compensators is designed. The simulation shows that using the switching control design method can not only improve the dynamic performance of the aircraft engine control system and reduce the switching times, but also guarantee the stability in some peculiar occasions. |
| Other Abstract | The aircraft engine multi-loop control system is described and the switching control theory is introduced to solve the regulating and protecting control problems in this paper. The aircraft engine multi-loop control system is firstly described and the control problems are formu-lated. Secondly, the theory of the smooth switching control is devoted and a new extended scheme for the smooth switching of a switched control system is introduced. Then, for the key technologies of aero-engines switching control, a design algorithm is presented which can determine which candidate controller should be put in feedback with the plant to achieve a desired performance and the procedure to design the aircraft engine multi-loop control system is detailed. The switching performance objectives and the switching scheme are given and a family of PID controllers and compensators is designed. The simulation shows that using the switching control design method can not only improve the dynamic performance of the aircraft engine control system and reduce the switching times, but also guarantee the stability in some peculiar occasions. |
| Keyword | Aircraft engine Compensatory controller Min/Max switching Multi-objectives control Smooth switching Switching scheme Motor vehicles. Aeronautics. Astronautics TL1-4050 |
| Indexed By | CSCD |
| Language | 英语 |
| Funding Project | [National Natural Science Foundation of China] ; [Innovation Plan of Aero Engine Complex System Safety by the Ministry of Education Chang Jiang Scholars of China] |
| CSCD ID | CSCD:5279795 |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://ir.imr.ac.cn/handle/321006/147516 |
| Collection | 中国科学院金属研究所 |
| Affiliation | 1.北京航空航天大学 2.中国科学院金属研究所 |
| Recommended Citation GB/T 7714 | Liu Xiaofeng,Shi Jing,Qi Yiwen,et al. Design for aircraft engine multi-objective controllers with switching characteristics[J]. Chinese Journal of Aeronautics,2014,27(5):1097-1110. |
| APA | Liu Xiaofeng,Shi Jing,Qi Yiwen,&Yuan Ye.(2014).Design for aircraft engine multi-objective controllers with switching characteristics.Chinese Journal of Aeronautics,27(5),1097-1110. |
| MLA | Liu Xiaofeng,et al."Design for aircraft engine multi-objective controllers with switching characteristics".Chinese Journal of Aeronautics 27.5(2014):1097-1110. |
| Files in This Item: | There are no files associated with this item. | |||||
Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.
Edit Comment