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Volumn 28, Issue 1, 2005, Pages 78-84

Control of unsteady aeroelastic system via state-dependent riccati equation method

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); MATHEMATICAL MODELS; MATRIX ALGEBRA; NONLINEAR CONTROL SYSTEMS; RICCATI EQUATIONS; UNSTEADY FLOW; VECTORS;

EID: 12744261530     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.6590     Document Type: Article
Times cited : (55)

References (34)
  • 3
    • 0141957140 scopus 로고    scopus 로고
    • Historical perspective on analysis and control of aeroelastic responses
    • Mukhopadhyay, V.,"Historical Perspective on Analysis and Control of Aeroelastic Responses," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 5, 2003, pp. 673-684.
    • (2003) Journal of Guidance, Control, and Dynamics , vol.26 , Issue.5 , pp. 673-684
    • Mukhopadhyay, V.1
  • 5
    • 0031268485 scopus 로고    scopus 로고
    • Adaptive control of aeroelastic instabilities in transonic flow and its scaling
    • Friedmann, P. P., Guillot, D., and Presente, E., "Adaptive Control of Aeroelastic Instabilities in Transonic Flow and Its Scaling," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 6, 1997, pp. 1190-1199.
    • (1997) Journal of Guidance, Control, and Dynamics , vol.20 , Issue.6 , pp. 1190-1199
    • Friedmann, P.P.1    Guillot, D.2    Presente, E.3
  • 6
    • 0034819199 scopus 로고    scopus 로고
    • Robust multivariable flutter suppression for the benchmark active control technology (BACT) wind-tunnel model
    • Waszak, M.R., "Robust Multivariable Flutter Suppression for the Benchmark Active Control Technology (BACT) Wind-Tunnel Model," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 1, 2001, pp. 147-153.
    • (2001) Journal of Guidance, Control, and Dynamics , vol.24 , Issue.1 , pp. 147-153
    • Waszak, M.R.1
  • 9
    • 0034274144 scopus 로고    scopus 로고
    • Transonic flutter suppression control law design and wind-tunnel test results
    • Mukhopadhyay, V., "Transonic Flutter Suppression Control Law Design and Wind-Tunnel Test Results," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 5, 2000, pp. 930-937.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.5 , pp. 930-937
    • Mukhopadhyay, V.1
  • 10
    • 0034276433 scopus 로고    scopus 로고
    • Passivity-based robust control with application to benchmark controls technology wing
    • Kelkar, A. G., and Joshi, S. M., "Passivity-Based Robust Control with Application to Benchmark Controls Technology Wing," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 5, 2000, pp. 938-947.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.5 , pp. 938-947
    • Kelkar, A.G.1    Joshi, S.M.2
  • 11
    • 0034274767 scopus 로고    scopus 로고
    • Comparing linear parameter-varying gain-scheduled control techniques for active flutter suppression
    • Barker, J. M., and Balas, G. J., "Comparing Linear Parameter-Varying Gain-Scheduled Control Techniques for Active Flutter Suppression," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 5, 2000, pp. 948-955.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.5 , pp. 948-955
    • Barker, J.M.1    Balas, G.J.2
  • 12
    • 0034314451 scopus 로고    scopus 로고
    • Active control of wind-tunnel model aeroelastic response using neural networks
    • Scott, R. C., and Pado, L. E., "Active Control of Wind-Tunnel Model Aeroelastic Response Using Neural Networks," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 6, 2000, pp. 1100-1108.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.6 , pp. 1100-1108
    • Scott, R.C.1    Pado, L.E.2
  • 13
    • 0034318042 scopus 로고    scopus 로고
    • Fundamental aeroservoelastic study combining unsteady computational fluid mechanics with adaptive control
    • Guillot, D. M., and Friedmann, P. P., "Fundamental Aeroservoelastic Study Combining Unsteady Computational Fluid Mechanics with Adaptive Control," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 6, 2000, pp. 1117-1126.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.6 , pp. 1117-1126
    • Guillot, D.M.1    Friedmann, P.P.2
  • 14
    • 0034316044 scopus 로고    scopus 로고
    • Control of a nonlinear aeroelastic system using euler-lagrange theory
    • Prasanth, R. K., and Mehra, R. K., "Control of a Nonlinear Aeroelastic System Using Euler-Lagrange Theory," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 6, 2000, pp. 1134-1139.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.6 , pp. 1134-1139
    • Prasanth, R.K.1    Mehra, R.K.2
  • 15
    • 0031683216 scopus 로고    scopus 로고
    • Nonlinear adaptive control of an aeroelastic system via geometric method
    • April
    • Ko, J., and Strganac, T. W.,"Nonlinear Adaptive Control of an Aeroelastic System via Geometric Method," AIAA Paper 98-1795, April 1998.
    • (1998) AIAA Paper , vol.98 , Issue.1795
    • Ko, J.1    Strganac, T.W.2
  • 16
    • 0032208512 scopus 로고    scopus 로고
    • Applied active control for a nonlinear aeroelastic structure
    • Block, J., and Strganac, T. M., "Applied Active Control for a Nonlinear Aeroelastic Structure," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 838-845.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.6 , pp. 838-845
    • Block, J.1    Strganac, T.M.2
  • 17
    • 0034316194 scopus 로고    scopus 로고
    • Identification and control of limit cycle oscillations in aeroelastic systems
    • Strganac, T. W., Ko, J., and Thompson, D. E., "Identification and Control of Limit Cycle Oscillations in Aeroelastic Systems," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 6, 2000, pp. 1127-1133.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.6 , pp. 1127-1133
    • Strganac, T.W.1    Ko, J.2    Thompson, D.E.3
  • 18
    • 0031275376 scopus 로고    scopus 로고
    • Nonlinear control of a prototypical wing section with torsional nonlinearity
    • Ko, J., Kurdila, A. J., and Strganac, T. W., "Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 6, 1997, pp. 1181-1189.
    • (1997) Journal of Guidance, Control, and Dynamics , vol.20 , Issue.6 , pp. 1181-1189
    • Ko, J.1    Kurdila, A.J.2    Strganac, T.W.3
  • 19
    • 0032166295 scopus 로고    scopus 로고
    • Stability and control of a structurally nonlinear aeroelastic system
    • Ko, J., and Strganac, T. W., "Stability and Control of a Structurally Nonlinear Aeroelastic System," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 5, 1998, pp. 718-725.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.5 , pp. 718-725
    • Ko, J.1    Strganac, T.W.2
  • 20
    • 0032647992 scopus 로고    scopus 로고
    • Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity
    • Ko., J., Strganac, T. W., and Kurdila, A. J., "Adaptive Feedback Linearization for the Control of a Typical Wing Section with Structural Nonlinearity," Nonlinear Dynamics, Vol. 18, No. 2, 1999, pp. 289-301.
    • (1999) Nonlinear Dynamics , vol.18 , Issue.2 , pp. 289-301
    • Ko, J.1    Strganac, T.W.2    Kurdila, A.J.3
  • 21
    • 0036175844 scopus 로고    scopus 로고
    • Computational and experimental investigation of limit cycle oscillations of nonlinear aeroelastic systems
    • Sheta, E., Harrand, V. J., Thompson, D. E., and Strganac, T. W., "Computational and Experimental Investigation of Limit Cycle Oscillations of Nonlinear Aeroelastic Systems," Journal of Aircraft, Vol. 39, No. 1, 2002, pp. 133-141.
    • (2002) Journal of Aircraft , vol.39 , Issue.1 , pp. 133-141
    • Sheta, E.1    Harrand, V.J.2    Thompson, D.E.3    Strganac, T.W.4
  • 22
    • 0032206717 scopus 로고    scopus 로고
    • Output feedback variable structure adaptive control of an aeroelastic system
    • Zeng Y., and Singh, S. N., "Output Feedback Variable Structure Adaptive Control of an Aeroelastic System," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 830-837.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.6 , pp. 830-837
    • Zeng, Y.1    Singh, S.N.2
  • 23
    • 0034314450 scopus 로고    scopus 로고
    • Adaptive output feedback control of a nonlinear aeroelastic structure
    • Xing, W., and Singh, S. N.,"Adaptive Output Feedback Control of a Nonlinear Aeroelastic Structure," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 6, 2000, pp. 1109-1116.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.6 , pp. 1109-1116
    • Xing, W.1    Singh, S.N.2
  • 24
    • 0036642247 scopus 로고    scopus 로고
    • Output feedback form and adaptive stabilization of a nonlinear aeroelastic system
    • Singh, S. N., and Wang, L., "Output Feedback Form and Adaptive Stabilization of a Nonlinear Aeroelastic System," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 4, 2002, pp. 725-732.
    • (2002) Journal of Guidance, Control, and Dynamics , vol.25 , Issue.4 , pp. 725-732
    • Singh, S.N.1    Wang, L.2
  • 25
    • 0038277132 scopus 로고    scopus 로고
    • Modular adaptive control of a nonlinear aeroelastic system
    • Singh, S. N., and Brenner, M.,"Modular Adaptive Control of a Nonlinear Aeroelastic System," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 3, 2003, pp. 443-451.
    • (2003) Journal of Guidance, Control, and Dynamics , vol.26 , Issue.3 , pp. 443-451
    • Singh, S.N.1    Brenner, M.2
  • 26
    • 12744276235 scopus 로고    scopus 로고
    • Stabilization of an aeroelastic system: A backstepping design
    • Aug.
    • Bhoir, N. G., and Singh, S. N., "Stabilization of an Aeroelastic System: A Backstepping Design," AIAA Paper 2003-5502, Aug. 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.5502
    • Bhoir, N.G.1    Singh, S.N.2
  • 27
    • 12744266689 scopus 로고    scopus 로고
    • Full envelope missile longitudinal autopilot design using the state-dependent riccati equation method
    • Aug.
    • Mracek, C. P., and Cloutier, J. R., "Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method," AIAA Paper 97-3767, Aug. 1997.
    • (1997) AIAA Paper , vol.97 , Issue.3767
    • Mracek, C.P.1    Cloutier, J.R.2
  • 28
    • 0032478466 scopus 로고    scopus 로고
    • Control designs for the nonlinear bench-mark problem via the state-dependent riccati equation method
    • April
    • Mracek, C. P., and Cloutier, J. R., "Control Designs for the Nonlinear Bench-Mark Problem via the State-Dependent Riccati Equation Method," International Journal of Robust Nonlinear Control, Vol. 8, April 1998, pp. 401-433.
    • (1998) International Journal of Robust Nonlinear Control , vol.8 , pp. 401-433
    • Mracek, C.P.1    Cloutier, J.R.2
  • 30
    • 84894426866 scopus 로고    scopus 로고
    • Nonlinear hybrid bank-to-turn/skid-to-turn autopilot design
    • Aug.
    • Cloutier, J. R., and Stansbery, D. T., "Nonlinear Hybrid Bank-to-Turn/Skid-to-Turn Autopilot Design," AIAA Paper 2001-5929, Aug. 2001.
    • (2001) AIAA Paper , vol.2001 , Issue.5929
    • Cloutier, J.R.1    Stansbery, D.T.2
  • 31
    • 0038066373 scopus 로고    scopus 로고
    • State feedback control of an aeroelastic system with structural nonlinearity
    • Singh, S. N., and Yim, W.,"State Feedback Control of an Aeroelastic System with Structural Nonlinearity," Aerospace Science and Technology, Vol. 7, No. 1, 2003, pp. 23-31.
    • (2003) Aerospace Science and Technology , vol.7 , Issue.1 , pp. 23-31
    • Singh, S.N.1    Yim, W.2
  • 32
    • 0344083636 scopus 로고    scopus 로고
    • State-dependent riccati equation for control of aeroelastic flutter
    • Tadi, M., "State-Dependent Riccati Equation for Control of Aeroelastic Flutter," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 6, 2003, pp. 914-917.
    • (2003) Journal of Guidance, Control, and Dynamics , vol.26 , Issue.6 , pp. 914-917
    • Tadi, M.1
  • 33
    • 0003222470 scopus 로고
    • General theory of aerodynamic instability and mechanism of flutter
    • Theodorsen, T., "General Theory of Aerodynamic Instability and Mechanism of Flutter," NACA Rept. 496, 1935.
    • (1935) NACA Rept. , vol.496
    • Theodorsen, T.1


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