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Volumn 219, Issue 4, 2005, Pages 341-359

Design and evaluation of a damage-tolerant flight control system

Author keywords

Reconfigurable control; Robust flight control; Sliding mode control

Indexed keywords

COMPUTER SIMULATION; CONTROL SYSTEMS; DEGREES OF FREEDOM (MECHANICS); SLIDING MODE CONTROL;

EID: 30344471546     PISSN: 09544100     EISSN: 09544100     Source Type: Journal    
DOI: 10.1243/095441005X7259     Document Type: Conference Paper
Times cited : (18)

References (11)
  • 1
    • 0003528698 scopus 로고    scopus 로고
    • Modular control law design for the innovative control effectors (ICE) tailless fighter aircraft configuration 101-3
    • AFRL-VA-WP-TR-1999-3057, Air Force Research Laboratory, June
    • Buffington, J. M. Modular control law design for the innovative control effectors (ICE) tailless fighter aircraft configuration 101-3. Final Report 5/1/97-5/1 /99, AFRL-VA-WP-TR-1999-3057, Air Force Research Laboratory, June 1999.
    • (1999) Final Report 5/1/97-5/1 /99
    • Buffington, J.M.1
  • 2
    • 0031274579 scopus 로고    scopus 로고
    • A unified theory for aircraft handling qualities and adverse aircraft-pilot coupling
    • November-December
    • Hess, R. A. A unified theory for aircraft handling qualities and adverse aircraft-pilot coupling. J. Guidance, Control, Dynamics, November-December 1997, 20(6), 1141-1148.
    • (1997) J. Guidance, Control, Dynamics , vol.20 , Issue.6 , pp. 1141-1148
    • Hess, R.A.1
  • 3
    • 0011084674 scopus 로고
    • Proposed incorporation of mission-oriented flying qualities into MIL-STD-1797A
    • Wright Laboratory, Wright-Patterson Air Force Base, Dayton, Ohio, October
    • Mitchell, D. G., Hoh, R. H., Aponso, B. L., and Klyde, D. H. Proposed incorporation of mission-oriented flying qualities into MIL-STD-1797A. Technical Report WL-TR-94-3162, Wright Laboratory, Wright-Patterson Air Force Base, Dayton, Ohio, October 1994.
    • (1994) Technical Report WL-TR-94-3162
    • Mitchell, D.G.1    Hoh, R.H.2    Aponso, B.L.3    Klyde, D.H.4
  • 4
    • 30344435746 scopus 로고    scopus 로고
    • Anon. Robust flight control design challenge, problem formulation and manual: The high incidence research model (HIRM)
    • April
    • Anon. Robust flight control design challenge, problem formulation and manual: the high incidence research model (HIRM). Technical Publication Garteur/TP-088-4, April 1997.
    • (1997) Technical Publication Garteur/TP-088-4
  • 5
    • 0038277134 scopus 로고    scopus 로고
    • Sliding mode control applied to reconfigurable flight control design
    • May-June
    • Hess, R. A. and Wells, S. R. Sliding mode control applied to reconfigurable flight control design. J. Guidance, Control, Dynamics, May-June 2003, 26(3), 452-462.
    • (2003) J. Guidance, Control, Dynamics , vol.26 , Issue.3 , pp. 452-462
    • Hess, R.A.1    Wells, S.R.2
  • 6
    • 0037939860 scopus 로고    scopus 로고
    • Multi-input/multi-output sliding mode control for a tailless fighter aircraft
    • May-June
    • Wells, S. R. and Hess, R A. Multi-input/multi-output sliding mode control for a tailless fighter aircraft. J. Guidance, Control, Dynamics, May-June 2003, 26(3), 463-473.
    • (2003) J. Guidance, Control, Dynamics , vol.26 , Issue.3 , pp. 463-473
    • Wells, S.R.1    Hess, R.A.2
  • 8
    • 19644397823 scopus 로고    scopus 로고
    • Tailless aircraft flight control using multiple time scale re-configurable sliding modes
    • Publication AIAA-99-4136, Portland, Oregon, 9-11 August (American Institute of Aeronautics and Astronautics, New York)
    • Shtessel, Y. B., Buffington, J. M., and Banda, S. S. Tailless aircraft flight control using multiple time scale re-configurable sliding modes. In Proceedings of the Guidance, Navigation, and Control Conference, Publication AIAA-99-4136, Portland, Oregon, 9-11 August 1999, pp. 966-976 (American Institute of Aeronautics and Astronautics, New York).
    • (1999) Proceedings of the Guidance, Navigation, and Control Conference , pp. 966-976
    • Shtessel, Y.B.1    Buffington, J.M.2    Banda, S.S.3
  • 10
    • 8644289374 scopus 로고    scopus 로고
    • Frequency-domain sliding mode design technique applied to the control of a ducted fan micro-air vehicle
    • Hess, R. A. and Ussery, T. Frequency-domain sliding mode design technique applied to the control of a ducted fan micro-air vehicle. J. Am. Helicopter Soc. 2004, 49(4), 457-467.
    • (2004) J. Am. Helicopter Soc. , vol.49 , Issue.4 , pp. 457-467
    • Hess, R.A.1    Ussery, T.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.