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Volumn 4, Issue 2, 1996, Pages 171-176

An analysis of the destabilizing effect of daisy chained rate-limited actuators

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; CONTROL SYSTEM ANALYSIS; NUMERICAL ANALYSIS; SYSTEM STABILITY;

EID: 0030104491     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.486343     Document Type: Article
Times cited : (78)

References (12)
  • 1
    • 0029191535 scopus 로고
    • High angle of attack short period flight control design with thrust vectoring
    • Seattle, WA, June
    • K. D. Hammett, W. C. Reigelsperger, and S. S. Banda, "High angle of attack short period flight control design with thrust vectoring," in Proc. 1995 Amer. Contr. Conf., Seattle, WA, June 1995, pp.-170-174.
    • (1995) Proc. 1995 Amer. Contr. Conf.
    • Hammett, K.D.1    Reigelsperger, W.C.2    Banda, S.S.3
  • 2
    • 0021132413 scopus 로고
    • Analysis of aircraft attitude control systems prone to pilot-induced oscillations
    • Jan.-Feb.
    • R. A. Hess, "Analysis of aircraft attitude control systems prone to pilot-induced oscillations," J. Guidance, vol. 7, no. 1, pp. 106-112, Jan.-Feb. 1984.
    • (1984) J. Guidance , vol.7 , Issue.1 , pp. 106-112
    • Hess, R.A.1
  • 3
    • 0001787057 scopus 로고
    • Report pinpoints factors leading to YF-22 crash
    • Nov. 9
    • M. A. Dornheim, "Report pinpoints factors leading to YF-22 crash," Aviation Week Space Technol., pp. 53-54, Nov. 9, 1992.
    • (1992) Aviation Week Space Technol. , pp. 53-54
    • Dornheim, M.A.1
  • 4
    • 0003138422 scopus 로고
    • Gripen control problems resolved through in-flight, ground simulations
    • June 18
    • J. M. Lenorovitz, "Gripen control problems resolved through in-flight, ground simulations," Aviation Week Space Technol., pp. 74-75, June 18, 1990.
    • (1990) Aviation Week Space Technol. , pp. 74-75
    • Lenorovitz, J.M.1
  • 5
  • 6
    • 0027628139 scopus 로고
    • Constrained control allocation
    • July-Aug.
    • W. C. Durham, "Constrained control allocation," J. Guidance, Contr., Dynamics, vol. 16, no. 4, pp. 717-725, July-Aug. 1993.
    • (1993) J. Guidance, Contr., Dynamics , vol.16 , Issue.4 , pp. 717-725
    • Durham, W.C.1
  • 7
    • 3743080229 scopus 로고
    • Aircraft control system rate limiting
    • Oct.-Dec.
    • L. H. Knotts, M. L. Parrag, and E. E. Ohmit, "Aircraft control system rate limiting," Cockpit, pp. 4-18, Oct.-Dec. 1993.
    • (1993) Cockpit , pp. 4-18
    • Knotts, L.H.1    Parrag, M.L.2    Ohmit, E.E.3
  • 8
    • 84959136443 scopus 로고    scopus 로고
    • Design of a flight control system for a highly maneuverable aircraft using μ synthesis
    • Monterey, CA
    • J. Reiner, G. J. Balas, and W. L. Garrard, "Design of a flight control system for a highly maneuverable aircraft using μ synthesis," in Proc. 1993 AIAA Guidance, Navigation, Contr. Conf., Monterey, CA, pp. 710-719.
    • Proc. 1993 AIAA Guidance, Navigation, Contr. Conf. , pp. 710-719
    • Reiner, J.1    Balas, G.J.2    Garrard, W.L.3
  • 10
    • 0003096706 scopus 로고
    • Dynamic inversion: An evolving methodology for flight control design
    • D. Enns, D. Bugajski, R. Hedrick, and G. Stein, "Dynamic inversion: An evolving methodology for flight control design," Int. J. Contr., vol. 59, no. 1, pp. 71-91, 1994.
    • (1994) Int. J. Contr. , vol.59 , Issue.1 , pp. 71-91
    • Enns, D.1    Bugajski, D.2    Hedrick, R.3    Stein, G.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.