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摘要
LQL (Linear quadratic L 2 bounded uncertainties) control method was applied to the aeroengine control system. The augmented LQL method was proposed, then the aeroengine control system was designed by using the method. Simulation of the control system in the flight envelope was performed, and excellent tracking performance and robustness were obtained.
- 出版日期2007
- 单位西北工业大学
