Robust Model Following Control Design for Missile Roll Autopilot

被引：0

作者：

Gezer, R. Berk ^{[1
]}

Kutay, Ali Turker ^{[2
]}

机构：

[1] Roketsan Missiles Inc, Engn Dev Directorate, Ankara, Turkey

[2] Middle E Tech Univ, Dept Aerosp Engn, TR-06531 Ankara, Turkey

来源：

2014 UKACC INTERNATIONAL CONFERENCE ON CONTROL (CONTROL) | 2014年

关键词：

Model following control; Robust control; Optimal control; Missile roll autopilot;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper presents a robust model following control method augmented with error integration and Luenberger observer for anti-air missile roll autopilot designed using optimal control laws. The design is shown to be robust to external disturbance, noisy measurements and sensor lags by frequency domain analysis. The regulation performance of the controller is presented by simulations.

引用

页码：7 / 12

页数：6

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