Some control strategies for a high-angle-of-attack missile autopilot

被引：58

作者：

Devaud, E

Siguerdidjane, H

Font, S

机构：

[1] Ecole Super Elect, Supelec, Serv Automat, F-91192 Gif Sur Yvette, France

[2] Aerospatiale, F-92323 Chatillon, France

来源：

CONTROL ENGINEERING PRACTICE | 2000年 / 8卷 / 08期

关键词：

missiles; nonlinear control; linearization; tracking; robustness;

D O I：

10.1016/S0967-0661(00)00013-7

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Recent interest in high maneuverability and stealth in missiles has triggered new investigations in estimating the potential and applicability of recent theoretical control methods as well as how they can meet industrial demands. Since the work presented here is closely related to an industrial application it is desirable to deal primarily with classical regulators. In this paper, two nonlinear methods are considered: 'Approximate feedback linearization' and the 'asymptotic output tracking' approach. Simulation results are given. (C) 2000 Elsevier Science Ltd. All rights reserved.

引用

页码：885 / 892

页数：8

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