|
|||||
|
|
Advanced optimization of gas turbine aero-engine transient performance using linkage-learning genetic algorithm: Part II,optimization in flight mission and controller gains correlation development |
|
| Institution: | 1. Aero Engine Test Department of Hunan Aviation Powerplant Research Institute, AECC, Zhuzhou 412002, China;2. Centre for Propulsion Engineering, School of Aerospace Transport and Manufacturing (SATM), Cranfield University, Cranfield MK43 0AL, UK |
| Abstract: | |
| Keywords: | Aeroengine control Control optimization Flight condition Flight mission simulation GA GTE LLGA Min-Max controller Robustness |
| 本文献已被 ScienceDirect 等数据库收录！ | |