Sliding Mode Fault Tolerant Control Allocation with Saturation Avoidance for a Blended Wing Body Aircraft

被引：0
|
作者：
Vile, Liam [1 ]
Alwi, Halim [1 ]
Edwards, Christopher [1 ]
机构：
[1] Univ Exeter, Coll Engn Math & Phys Sci, Exeter EX4 4QF, Devon, England
来源：
2019 IEEE 58TH CONFERENCE ON DECISION AND CONTROL (CDC) | 2019年
关键词：
STABILITY;
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 proposes a sliding mode controller with priority weighted control allocation and a saturation mitigating component. The control scheme aims to reduce degradation to the system's performance in the presence of faults and failures whilst keeping the actuators within their physical limits. Simulation results from a model of a blended wing body's lateral dynamics demonstrate the effectiveness of the scheme.
引用
收藏
页码：4958 / 4963
页数：6
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