Design Of VSC For Overload Control In High Angle-of-attack Missile

被引：0

作者：

Liang, Xuechao ^{[1
]}

Yang, Jun ^{[1
]}

Qiu, Feng ^{[2
]}

机构：

[1] Northwest Polytech Univ, Sch Astronaut, Xian 710072, Shaanxi Provinc, Peoples R China

[2] Chinese Peoples Liberat Arm, 96361 troop, Xining 810100, Peoples R China

来源：

2013 IEEE INTERNATIONAL CONFERENCE OF IEEE REGION 10 (TENCON) | 2013年

关键词：

high angle-of-attack; sliding mode; parameter perturbation; air defence missile;

D O I：

暂无

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

The purpose of this paper is to design a overload control system of the high angle-of-attack missile. First, the problems of the high angle-of-attack missile in flight process and the advantages of the variable structure control theory are analyzed. Then, the longitudinal motion model is built. Based on the accelerometer flight control system, the sliding mode controller and the control law are designed. The performance of the controller is tested under parameter perturbation in simulink. The result shows that the variable structure autopilot of overload is superior to the traditional design under the condition of the high angle-of-attack flight.

引用

页数：4