Tolerant Control Scheme Applied to an Aerospace Launcher

被引：0

作者：

Zbiri, Nabila ^{[1
]}

Manseur, Zohra ^{[2
]}

Boulaabi, Iskander ^{[3
]}

机构：

[1] Lab Informat Biol Integrat & Syst Complexes IBISC, Evry, France

[2] SUNY Coll Oswego, Dept Math, Oswego, NY USA

[3] Ecole Super Sci & Tech Tunis, Tunis, Tunisia

来源：

PROCEEDINGS OF THE FIRST INTERNATIONAL CONFERENCE ON PERFORMANCE, SAFETY AND ROBUSTNESS IN COMPLEX SYSTEMS AND APPLICATIONS (PESARO 2011) | 2011年

关键词：

aerospace launcher; observer; stability; fault detection; control;

D O I：

暂无

中图分类号：

TP301 [理论、方法];

学科分类号：

081202 ;

摘要：

Autonomous aerospace launchers must carry out their missions safely because any accident can lead to important or dramatic consequences. It is essential to develop robust control solutions that guarantee optimal performances even when failures occur during these missions. The main objective of this paper is to present the development of a fault-tolerant control design in the case of an aerospace launcher. The method consists of defining and carrying out effective procedures for early detection of some critical situations and providing an adequate control that maintains the safe behaviour of the launcher. The improved control performance is obtained by using a sliding mode observer for a robust reconstruction of an actuator fault. This reconstruction is used then to generate an added signal in the initial control law that compensates for the effect of the faults. Simulation results will show the efficiency of the proposed method.

引用

页码：35 / 41

页数：7

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