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Volumn 29, Issue 3, 2006, Pages 635-642

Fault-tolerant structured adaptive model inversion control

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; CONTROL EQUIPMENT; DYNAMICS; MATHEMATICAL MODELS; PROBLEM SOLVING; UNCERTAIN SYSTEMS;

EID: 33744724319     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.15244     Document Type: Article
Times cited : (45)

References (22)
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    • Boskovic, J.D.1    Mehra, R.K.2
  • 3
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    • Accommodation of failures in the F-16 aircraft using adaptive control
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    • Reconfigurable systems for tailless fighter aircraft RESTORE
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    • "Reconfigurable Systems for Tailless Fighter Aircraft RESTORE," Scientific and Technical Repts., System Design Rept., Contract Data Requirement List (CDRL) Sequence A007 F33615-96-C-3612, Boeing Phantom Works, St. Louis, MO, May 1998.
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    • Boskovic, J. D., and Mehra, R. K., "Robust Fault-Tolerant Control Design for Aircraft Under State-Dependent Disturbances," AIAA Paper 2003-5490, Aug. 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.5490
    • Boskovic, J.D.1    Mehra, R.K.2
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    • Adaptive realization of linear closed-loop tracking dynamics in the presence of large system model errors
    • Schaub, H., Akella, M. R., and Junkins, J. L., "Adaptive Realization of Linear Closed-Loop Tracking Dynamics in the Presence of Large System Model Errors," Journal of Astronautical Sciences, Vol. 48, No. 4, 2000, pp. 537-551.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.