您当前的位置:
首页 >
文章列表页 >
ADAPTIVE MODELLING TECHNIQUE FOR AEROENGINE
更新时间:2026-07-07
    • ADAPTIVE MODELLING TECHNIQUE FOR AEROENGINE

    • Vol. 14, Issue 4, (1999)
    • Published:1999

    移动端阅览

  • Duan Shoufu, Qi Wenkai, Gao Deping. ADAPTIVE MODELLING TECHNIQUE FOR AEROENGINE[J]. 1999, 14(4). DOI:

  •  
  •  
icon
试读结束,您可以激活您的VIP账号继续阅读。
去激活 >
icon
试读结束,您可以通过登录账户,到个人中心,购买VIP会员阅读全文。
已是VIP会员?
去登录 >

0

Views

411

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

Adaptive global fast non-singular Terminal sliding mode control for aero-engine
Application of adaptive second-order dynamic terminal sliding mode control to near space vehicle
Study on the characteristics of bipropellant-fueled pulse rocket engine with high combustion chamber pressure
Multivariable adaptive decoupling control based on auto-tuning neurons for aeroengine
Adaptive control study and experimental validation of a micro turbine engine

Related Author

WU Yong
WANG Li-guo
REN Li-tong
ZHANG Bo
XIE Shou-sheng
MIAO Zhuo-guang
JIANG Chang-sheng
PU Ming

Related Institution

Army Aviation Research Institute, the Headquarters of the General staff, the Chinese People's Liberation Army
The Unit 61769, the Chinese People's Liberation Army, LÜliang Shanxi
The Unit 95961, the Chinese People's Liberation Amay
Aeronautics and Astronautics Engineering College, Air Force Engineering University
Laboratory of Pattern Recognition and Intelligent Systems, College of Automation Engineering, Nanjing University of Aeronautics and Astronautics
0