TY - GEN
T1 - Design of missile flight control system based on variable structure control theory
AU - Lou, Jiang
AU - Cai, Zhihao
AU - Zhao, Jiang
AU - Wu, Kun
AU - Wang, Yingxun
N1 - Publisher Copyright:
© 2017 Technical Committee on Control Theory, CAA.
PY - 2017/9/7
Y1 - 2017/9/7
N2 - Flight control system plays an important role in the process of missile designing. The quality of flight control system will affect the missile's performance significantly. In this article, we design a flight control system using variable structure control theory. Firstly, we establish a mathematical model of the missile and the basic content of variable structure control theory is introduced. Next chapter are mainly aiming at designing the control system of the missile's normal overload. Consequently, the linearized missile's normal overload is designed by using the mathematical model in chapter two. Then the variable structure controller is designed. In addition, we use the variable structure controller to optimize the linear normal load control system. The numerical simulation of two different control methods are given. And the result illustrate that the robustness of the control system based on variable structure theory are better.
AB - Flight control system plays an important role in the process of missile designing. The quality of flight control system will affect the missile's performance significantly. In this article, we design a flight control system using variable structure control theory. Firstly, we establish a mathematical model of the missile and the basic content of variable structure control theory is introduced. Next chapter are mainly aiming at designing the control system of the missile's normal overload. Consequently, the linearized missile's normal overload is designed by using the mathematical model in chapter two. Then the variable structure controller is designed. In addition, we use the variable structure controller to optimize the linear normal load control system. The numerical simulation of two different control methods are given. And the result illustrate that the robustness of the control system based on variable structure theory are better.
KW - flight control system
KW - linearization control
KW - variable structure control
UR - https://www.scopus.com/pages/publications/85032223479
U2 - 10.23919/ChiCC.2017.8027958
DO - 10.23919/ChiCC.2017.8027958
M3 - 会议稿件
AN - SCOPUS:85032223479
T3 - Chinese Control Conference, CCC
SP - 3841
EP - 3846
BT - Proceedings of the 36th Chinese Control Conference, CCC 2017
A2 - Liu, Tao
A2 - Zhao, Qianchuan
PB - IEEE Computer Society
T2 - 36th Chinese Control Conference, CCC 2017
Y2 - 26 July 2017 through 28 July 2017
ER -