Adaptive actuator failure compensation for parametric strict feedback systems and an aircraft application

被引：274
|
作者：
Tang, XD
Tao, G [1 ]
Joshi, SM
机构：
[1] Univ Virginia, Dept Elect & Comp Engn, Charlottesville, VA 22903 USA
[2] NASA, Langley Res Ctr, Hampton, VA 23681 USA
来源：
AUTOMATICA | 2003年 / 39卷 / 11期
关键词：
actuator failure; adaptive control; aircraft dynamics; failure compensation; nonlinear systems; output tracking; stability;
D O I：
10.1016/S0005-1098(03)00219-X
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Adaptive actuator failure compensation for parametric-strict-feedback systems is studied under different system structure conditions. Adaptive state feedback control schemes are developed, which ensure asymptotic output tracking and closed-loop signal boundedness. An adaptive control scheme is applied to a twin otter aircraft longitudinal nonlinear dynamics model in the presence of unknown failures in a two-segment elevator servomechanism. Simulation results verify the effectiveness of adaptive actuator failure compensation for desired system performance. (C) 2003 Elsevier Ltd. All rights reserved.
引用
收藏
页码：1975 / 1982
页数：8
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