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Volumn 17, Issue 2, 1996, Pages 123-140

Linear quadratic optimal model-following control of a helicopter in hover

Author keywords

Helicopter flight control; Linear quadratic optimal control; Model following control; Robustness; Sensitivity

Indexed keywords

CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; FLIGHT DYNAMICS; HELICOPTERS; LINEAR CONTROL SYSTEMS; MATHEMATICAL MODELS; MOTION CONTROL; ROBUSTNESS (CONTROL SYSTEMS); SENSITIVITY ANALYSIS;

EID: 0030123347     PISSN: 01432087     EISSN: None     Source Type: Journal    
DOI: 10.1002/(SICI)1099-1514(199604/06)17:2<123::AID-OCA568>3.0.CO;2-3     Document Type: Article
Times cited : (14)

References (12)
  • 1
    • 4344684655 scopus 로고
    • An in-flight investigation into the relationships among control sensitivity, control bandwidth and disturbance rejection bandwidth using a variable stability helicopter
    • Amsterdam, Paper 61
    • Baillie, S. W. and J. M. Morgan, 'An in-flight investigation into the relationships among control sensitivity, control bandwidth and disturbance rejection bandwidth using a variable stability helicopter', Proc. 15th Eur. Rotorcraft Forum, Amsterdam, 1989, Paper 61.
    • (1989) Proc. 15th Eur. Rotorcraft Forum
    • Baillie, S.W.1    Morgan, J.M.2
  • 2
    • 0022276491 scopus 로고
    • The application of model control theory to the single rotor helicopter
    • London, Paper 78
    • Parry, D. L. K. and D. J. Murray-Smith, 'The application of model control theory to the single rotor helicopter', Proc. 11th Eur. Rotorcraft Forum, London, 1989. Paper 78.
    • (1989) Proc. 11th Eur. Rotorcraft Forum
    • Parry, D.L.K.1    Murray-Smith, D.J.2
  • 4
    • 5544284103 scopus 로고
    • Design of flight control systems to meet rotorcraft handling qualities specifications
    • New Orleans, LA, 1991, AIAA, New York
    • Low, E. and W. Garrard, 'Design of flight control systems to meet rotorcraft handling qualities specifications', Proc. AIAA Guidance Navigation and Control Conf., New Orleans, LA, 1991, AIAA, New York, 1991, pp. 1381-1391.
    • (1991) Proc. AIAA Guidance Navigation and Control Conf. , pp. 1381-1391
    • Low, E.1    Garrard, W.2
  • 6
    • 0342956084 scopus 로고
    • The National Aeronautical Establishment airborne simulation facility
    • NAE Misc. #58
    • Sattler, D. E., 'The National Aeronautical Establishment airborne simulation facility', NAE Misc. #58, presented at 31st Ann. CASI Gen. Meet., 1984.
    • (1984) 31st Ann. CASI Gen. Meet.
    • Sattler, D.E.1
  • 8
    • 0019531761 scopus 로고
    • Multivariable feedback design: Concepts for a modem/classical synthesis
    • Doyle, J. C. and G. Stein, 'Multivariable feedback design: concepts for a modem/classical synthesis', IEEE Tran. Automatic Control, AC-26, 4-16 (1981).
    • (1981) IEEE Tran. Automatic Control , vol.AC-26 , pp. 4-16
    • Doyle, J.C.1    Stein, G.2
  • 9
    • 0016973773 scopus 로고
    • Model-following in linear quadratic optimization
    • Kreindler, E. and D. Rothschild, 'Model-following in linear quadratic optimization', AIAA J., 14, 835-842 (1976).
    • (1976) AIAA J. , vol.14 , pp. 835-842
    • Kreindler, E.1    Rothschild, D.2
  • 11
    • 0015331778 scopus 로고
    • Design of desirable airplane handling qualities via optimal control
    • Kreichbaum, G. K. L. and R. W. Stineman, 'Design of desirable airplane handling qualities via optimal control', J. Aircraft, 9, 365-369 (1972).
    • (1972) J. Aircraft , vol.9 , pp. 365-369
    • Kreichbaum, G.K.L.1    Stineman, R.W.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.