作者: G. Schram , B. Verschoor , J.M. Sousa , H.B. Verbruggen
DOI: 10.1109/FUZZY.1997.616354
关键词:
摘要: Reconfiguration of flight control systems can be performed by using multiple controllers for anticipated failures. The use fuzzy logic is studied a simple implementation this approach. As test case, civil aircraft benchmark problem considered. results show that two pairs rule bases, the specification normal conditions as well in case an engine failure are fulfilled. Smooth switching between modes achieved membership functions.