Switching Control Design for A Hypersonic Flight Vehicle

被引：0
|
作者：
Tan, Shuping [1 ]
Li, Zhibin [1 ]
机构：
[1] Natl Lab Space Intelligent Control, Beijing 100190, Peoples R China
来源：
2010 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-5 | 2010年
关键词：
Hypersonic Flight Vehicle; Switching Control; Adaptive Switching Law; Stability; STABILIZATION;
D O I：
10.1109/CCDC.2010.5498526
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
An adaptive switching controller is designed and analyzed for the longitudinal dynamics of a generic hypersonic air vehicle in the whole cruise phase rather than a trimmed working condition. This model is nonlinear, multivariable and unstable. The adaptive controller presented in this paper consists of a local linearization method, an adaptive switching law and a nonlinear feedback control law. Furthermore, a theorem is obtained that the closed-loop system under the adaptive switching control is stable.
引用
收藏
页码：3568 / 3573
页数：6
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