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Volumn 3, Issue , 2006, Pages 1973-1994

Closed-loop evaluation of an integrated failure identification and fault tolerant control system for a transport aircraft

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; COMPUTER SOFTWARE; FLIGHT DYNAMICS; IDENTIFICATION (CONTROL SYSTEMS); ROBUSTNESS (CONTROL SYSTEMS); UNCERTAIN SYSTEMS;

EID: 33845771286     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-6310     Document Type: Conference Paper
Times cited : (20)

References (20)
  • 2
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    • Adaptive linear parameter varying control synthesis for actuator failure
    • Sept.-Oct.
    • Shin, J-Y., N.B. Eva, and Belcastro, C., "Adaptive Linear Parameter Varying Control Synthesis for Actuator Failure," Journal of Guidance, Control, and Dynamics, Vol. 27, Sept.-Oct. 2004, pp. 787-794.
    • (2004) Journal of Guidance, Control, and Dynamics , vol.27 , pp. 787-794
    • Shin, J.-Y.1    Eva, N.B.2    Belcastro, C.3
  • 3
    • 0036061309 scopus 로고    scopus 로고
    • Uncertainty modeling for robustness analysis of failure detection and accommodation systems
    • American Control Conference
    • Belcastro, C. and Chang, B-C., "Uncertainty Modeling for Robustness Analysis of Failure Detection and Accommodation Systems," in IEEE American Control Conference, Vol. 6, American Control Conference, 2002, pp. 4776-4782.
    • (2002) IEEE American Control Conference , vol.6 , pp. 4776-4782
    • Belcastro, C.1    Chang, B.-C.2
  • 4
    • 29744446871 scopus 로고    scopus 로고
    • Airborne subscale transport aircrat research testbed- aircraft model development
    • AIAA-2005-6432, AIAA
    • Jordan, T., Langford, W., and Hill, J., "Airborne Subscale Transport Aircrat Research Testbed- Aircraft Model Development," in AIAA Guidance. Navigation and Control Conference, AIAA-2005-6432, AIAA, 2005.
    • (2005) AIAA Guidance. Navigation and Control Conference
    • Jordan, T.1    Langford, W.2    Hill, J.3
  • 8
    • 0022199472 scopus 로고
    • A mu-test for robustness analysis of real-parameter variation problem
    • Morton, B. and McAfoos, R., "A Mu-test for Robustness Analysis of Real-parameter Variation Problem," in Proceedings of the American Control Conference, Vol. 1, 1985, pp. 135-138.
    • (1985) Proceedings of the American Control Conference , vol.1 , pp. 135-138
    • Morton, B.1    McAfoos, R.2
  • 9
    • 0022304964 scopus 로고
    • New application of mu to real-parameter variations problems
    • (Fort Lauderdale, FL)
    • Morton, B., "New Application of mu to real-parameter Variations Problems," in IEEE Conference on Decision and Control, (Fort Lauderdale, FL), 1985.
    • (1985) IEEE Conference on Decision and Control
    • Morton, B.1
  • 13
    • 19644371323 scopus 로고    scopus 로고
    • Linear parameter-varying detection filter design for a boeing 747-100/200 aircraft
    • Szaszi, I., Marcos, A., Balas, G., and Bokor, J., "Linear Parameter-Varying Detection Filter Design for a Boeing 747-100/200 Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 28, No. 3, 2005, pp. 461-470.
    • (2005) Journal of Guidance, Control, and Dynamics , vol.28 , Issue.3 , pp. 461-470
    • Szaszi, I.1    Marcos, A.2    Balas, G.3    Bokor, J.4
  • 17
    • 85086612765 scopus 로고    scopus 로고
    • Linear parameter varying modeling of the boeing 747-100/200 longitudinal motion
    • AIAA-01-4347, American Institute of Aeronautics and Astronautics, (Montreal, Canada), Aug.
    • Marcos, A. and Balas, G., "Linear Parameter Varying Modeling of the Boeing 747-100/200 Longitudinal Motion," in AIAA Guidance, Navigation and Control Conference, AIAA-01-4347, American Institute of Aeronautics and Astronautics, (Montreal, Canada), Aug. 2001.
    • (2001) AIAA Guidance, Navigation and Control Conference
    • Marcos, A.1    Balas, G.2
  • 19
    • 0036856806 scopus 로고    scopus 로고
    • Blending methodology of linear parmeter varying control synthesis of F-16 aircraft system
    • Shin, J-Y., Balas, G.J., and Kaya, M.A., "Blending Methodology of Linear Parmeter Varying Control Synthesis of F-16 Aircraft System," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 6, 2002, pp. 1040-1048.
    • (2002) Journal of Guidance, Control, and Dynamics , vol.25 , Issue.6 , pp. 1040-1048
    • Shin, J.-Y.1    Balas, G.J.2    Kaya, M.A.3
  • 20
    • 19944369435 scopus 로고    scopus 로고
    • Quasi-linear parameter varying representation over non-trim region
    • AIAA-2004-5423, (Providence, Rhode Island), AIAA
    • Shln, J-Y. and Belcastro, C., "Quasi-Linear Parameter Varying Representation over Non-trim Region," in AIAA Guidance, Navigation and Control Conference, AIAA-2004-5423, (Providence, Rhode Island), 2004, AIAA.
    • (2004) AIAA Guidance, Navigation and Control Conference
    • Shln, J.-Y.1    Belcastro, C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.