Minimum eigenvalue based adaptive fault compensation for hypersonic vehicles

被引：0
|
作者：
Ma, Yajie [1 ]
Jiang, Bin [1 ]
Ren, Hao [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Peoples R China
来源：
JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS | 2023年 / 34卷 / 02期
基金：
中国国家自然科学基金;
关键词：
Actuators; Eigenvalues and eigenfunctions; Attitude control; Vehicle dynamics; Hypersonic vehicles; Fault tolerant systems; Control design; actuator fault; adaptive compensation; hypersonic vehicle; minimum eigenvalue; ACTUATOR FAILURE COMPENSATION; TOLERANT CONTROL; TRACKING CONTROL; SYSTEM;
D O I：
10.23919/JSEE.2023.000039
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The attitude tracking control problem is addressed for hypersonic vehicles under actuator faults that may cause an uncertain time-varying control gain matrix. An adaptive compensation scheme is developed to ensure system stability and asymptotic tracking properties, including a kinematic control signal and a dynamic control signal. To deal with the uncertainties of the control gain matrix, a new positive definite one is constructed. The minimum eigenvalue of such a new control gain matrix is estimated. Simulation results of application to an X-33 vehicle model verify the effectiveness of the proposed minimum eigenvalue based adaptive fault compensation scheme.
引用
收藏
页码：492 / 500
页数：9
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