Chinese
您当前的位置：
首页 >
文章列表页 >
Control system design for engine of a small-size unmanned helicopter
更新时间：2026-07-07

    • Control system design for engine of a small-size unmanned helicopter

    • Vol. 22, Issue 12, (2007)

    • Published：2007

    移动端阅览

  • WANG Xiao-qing, HUANG Yi-ming, YANG Yi-dong, et al. Control system design for engine of a small-size unmanned helicopter[J]. 2007, 22(12). 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

493

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

Control strategy for piston ECU engine of small-size unmanned helicopter in overrunning stage
Piston engine speed H_∞ dynamic output feedback regulation based on LMI
Intake and exhaust system optimization of UAV piston engine
Prediction method on equivalent thermal conductivity coefficient of plain braided C/SiC composites material based on finite element method
Aerodynamic characteristics of design Mach number of 5 two-dimensional inlet with mixed-compression under typical condition

Related Author

HUANG Yi-min
SHAO Jin-ju
WEI Min-xiang
WEN Wei-dong
胡春明
郝蒙蒙
LU Si-da
GAO Xi-guang

Related Institution

College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
天津大学 天津内燃机研究所
天津大学 机械工程学院 内燃机燃烧学国家重点实验室
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
Department of Power and Propulsion, School of Engineering, Cranfield University, Bedfordshire MK4
0