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Volumn 6, Issue PART 1, 2006, Pages 819-824

Fault tolerant control of the boeing 747 short-period mode using the admissible model matching technique

Author keywords

Actuator fault accommodation; Admissible model matching; Fault tolerant control

Indexed keywords

FAULT DETECTION; FAULT TOLERANCE; FAULT TOLERANT COMPUTER SYSTEMS; PLANT MANAGEMENT;

EID: 79961143213     PISSN: 14746670     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.3182/20060829-4-cn-2909.00136     Document Type: Conference Paper
Times cited : (11)

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  • 4
    • 0000775115 scopus 로고
    • Reconfigurable control system design via perfect model following
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  • 5
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  • 6
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.