Multiple-Model Switching Control based Adaptive Failure Compensation for Hypersonic Vehicles

被引：0

作者：

Ma, Yajie ^{[1
]}

Jiang, Bin ^{[1
]}

Tao, Gang ^{[2
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjiang, Peoples R China

[2] Univ Virginia, Dept Elect & Comp Engn, Charlottesville, VA USA

来源：

2017 CHINESE AUTOMATION CONGRESS (CAC) | 2017年

基金：

中国国家自然科学基金;

关键词：

Adaptive compensation; Hypersonic vehicles; Multiple-model switching control; Stuck actuator failure;

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 develops a multiple-model switching control based adaptive failure compensation scheme lOr hypersonic vehicles with some stuck actuators. The system uncertainties, caused by failures and unknown inertia parameters, arc first parameterized. Then multiple adaptive dynamic estimators are designed, based on which, multiple adaptive control signals are designed using an error transformation. Finally, a control switching mechanism is established to select an appropriate control signal as the applied one. Simulation results on an X33 vehicle model are given to demonstrate the its effectiveness.

引用

页码：6701 / 6706

页数：6

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