Old Web
English
Sign In
Acemap
>
Paper
>
Four-Loop Feedback Control System with Integrator Design for Hypersonic Cruise Missile
Four-Loop Feedback Control System with Integrator Design for Hypersonic Cruise Missile
2017
Hongyang Xu
Yunfeng Yu
Xiaowen Guo
Fan Wang
Keywords:
Cruise missile
Hypersonic speed
Integrator
Control theory
Control system
Control engineering
Engineering
Computer science
feedback control
Correction
Source
Cite
Save
Machine Reading By IdeaReader
3
References
2
Citations
NaN
KQI
[]