Aero engine thrust estimator design based on kernel method

被引：0
|
作者：
Liu, Yi-Nan [1 ]
Zhang, Sheng-Xiu [1 ]
Zhang, Chao [1 ]
机构：
[1] Department of Automatic Control Engineering, The Second Artillery Engineering University, Xi'an 710025, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2013年 / 34卷 / 06期
关键词：
17;
D O I：
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中图分类号：
学科分类号：
摘要：
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页码：829 / 835
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