Differential flatness based control of Glide-reentry anti-vessel missile engineless part
Proceedings of the 30th Chinese Control Conference, CCC 2011（2011）
摘要
Nonlinear inverse dynamic controller based on differential flatness was designed for Glide-reentry anti-vessel missile terminal engineless part. Aerodynamic data was processed to make the missile model flat. Brake rudder was introduced to control terminal energy and fulfill the requirement of flatness. © 2011 Chinese Assoc of Automati.
更多查看译文
关键词
anti-vessel missile,differential flatness,glide-reentry,nonlinear inverse dynamic,nonlinear systems,trajectory,atmospheric modeling,vehicle dynamics,aerodynamics
AI 理解论文
溯源树
样例
生成溯源树，研究论文发展脉络
Chat Paper
正在生成论文摘要