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Volumn 17, Issue 3, 1994, Pages 458-465

Approximate recovery of H∞ loop shapes using fixed-order dynamic compensation

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT INSTRUMENTS; DESIGN; FLIGHT DYNAMICS; MATHEMATICAL MODELS; TRANSFER FUNCTIONS;

EID: 0028425427     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.21221     Document Type: Article
Times cited : (3)

References (15)
  • 1
    • 0025401280 scopus 로고
    • An Approximate Loop Transfer Recovery Method for Designing Fixed Order Compensators
    • Calise, A. J., and Prasad, J. V. R., “An Approximate Loop Transfer Recovery Method for Designing Fixed Order Compensators,” Journal of Guidance, Control, and Dynamics, Vol. 13, No. 2, 1990, pp. 297-302.
    • (1990) Journal of Guidance, Control, and Dynamics , vol.13 , Issue.2 , pp. 297-302
    • Calise, A.J.1    Prasad, J.V.R.2
  • 2
    • 0023847081 scopus 로고
    • Fixed Order Dynamic Compensation for Multivariable Linear Systems
    • Kramer, F. S., and Calise, A. J., “Fixed Order Dynamic Compensation for Multivariable Linear Systems,” Journal of Guidance, Control, and Dynamics, Vol. 11, No. 1, 1988, pp. 80-85.
    • (1988) Journal of Guidance, Control, and Dynamics , vol.11 , Issue.1 , pp. 80-85
    • Kramer, F.S.1    Calise, A.J.2
  • 3
    • 0019531761 scopus 로고
    • Multivariable Feedback Design: Concepts for a Classical/Modem Synthesis
    • Feb
    • Doyle, J. C., and Stein, G., “Multivariable Feedback Design: Concepts for a Classical/Modem Synthesis,” IEEE Transactions on Automatic Control, Vol. AC-26, Feb. 1981, pp. 4-16.
    • (1981) IEEE Transactions on Automatic Control , vol.AC-26 , pp. 4-16
    • Doyle, J.C.1    Stein, G.2
  • 4
    • 85003260832 scopus 로고
    • Output Loop Transfer Recovery for Fixed Order Dynamic Compensators
    • American Control Conference, San Diego, CA, May, also, (to be published)
    • Calise, A. J., and Byms, E. V., Jr., “Output Loop Transfer Recovery for Fixed Order Dynamic Compensators,” American Control Conference, San Diego, CA, May 1990; also Optimal Control Theory and Applications (to be published).
    • (1990) Optimal Control Theory and Applications
    • Calise, A.J.1    Byms, E.V.2
  • 6
    • 0023349261 scopus 로고
    • Disturbance Attenuation and H„ Optimization: A Design Method Based on the Algebraic Riccati Equation
    • May
    • Petersen, I. R., “Disturbance Attenuation and H„ Optimization: A Design Method Based on the Algebraic Riccati Equation,” IEEE Transactions on Automatic Control, Vol. AC-32, May 1987, pp. 427-429.
    • (1987) IEEE Transactions on Automatic Control , vol.AC-32 , pp. 427-429
    • Petersen, I.R.1
  • 8
    • 0024628058 scopus 로고
    • LQG Control with an Performance Bound: A Riccati Equation Approach
    • March
    • Bernstein, D. S., and Fladdad, W. M., “LQG Control with an Performance Bound: A Riccati Equation Approach,” IEEE Transactions on Automatic Control, Vol. AC-34, March 1989, pp. 293-305.
    • (1989) IEEE Transactions on Automatic Control , vol.AC-34 , pp. 293-305
    • Bernstein, D.S.1    Fladdad, W.M.2
  • 9
    • 0021531885 scopus 로고
    • The Optimal Projection Equations for Fixed Order Dynamic Compensation
    • Nov
    • Hyland, D. C., and Bernstein, D. S., “The Optimal Projection Equations for Fixed Order Dynamic Compensation,” IEEE Transactions on Automatic Control, Vol. AC-29, Nov. 1984, pp. 1034-1037.
    • (1984) IEEE Transactions on Automatic Control , vol.AC-29 , pp. 1034-1037
    • Hyland, D.C.1    Bernstein, D.S.2
  • 10
    • 85003361447 scopus 로고
    • High Performance H2 and Designs for the Supermaneuverable F-18/HARV Fighter Aircraft
    • Voulgaris, P., and Valavani, L., “High Performance H2 and Designs for the Supermaneuverable F-18/HARV Fighter Aircraft,” Journal of Guidance, Control, and Dynamics, Vol. 14, No. 1, 1991, pp. 157-165.
    • (1991) Journal of Guidance, Control, and Dynamics , vol.14 , Issue.1 , pp. 157-165
    • Voulgaris, P.1    Valavani, L.2
  • 12
    • 0016093440 scopus 로고
    • A Concise Derivation of Optimal Constant Limited State Feedback Gains
    • Aug
    • Mendel, J. M., “A Concise Derivation of Optimal Constant Limited State Feedback Gains,” IEEE Transactions on Automatic Control, Vol. AC-19, Aug. 1974, pp. 447, 448.
    • (1974) IEEE Transactions on Automatic Control , vol.AC-19
    • Mendel, J.M.1
  • 13
    • 85003313195 scopus 로고
    • Ph. D. Dissertation, School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA, May
    • Byms, E. V., Jr., “Design and Analysis of Robust Fixed Order Dynamic Compensators,” Ph. D. Dissertation, School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA, May 1991.
    • (1991) Design and Analysis of Robust Fixed Order Dynamic Compensators
    • Byms, E.V.1
  • 14
    • 0022118227 scopus 로고
    • Convergence of a Numerical Algorithm for Calculating Optimal Output Feedback Gains
    • Sept
    • Moerder, D. D., and Calise, A. J., “Convergence of a Numerical Algorithm for Calculating Optimal Output Feedback Gains,” IEEE Transactions on Automatic Control, Vol. AC-30, Sept. 1985, pp. 900-903.
    • (1985) IEEE Transactions on Automatic Control , vol.AC-30 , pp. 900-903
    • Moerder, D.D.1    Calise, A.J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.