Stability analysis of reconfigurable and gain scheduled flight control systems using LMIs

1998 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1998, Pages 118-126

  Wise, Kevin A ^a   Sedwick, Jack L ^a  

^a AIR FORCE OFFICE OF SCIENTIFIC RESEARCH   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; CONTROL SYSTEM ANALYSIS; FLIGHT CONTROL SYSTEMS; ITERATIVE METHODS; LINEAR MATRIX INEQUALITIES; SCHEDULING; TIME VARYING CONTROL SYSTEMS;

ADAPTIVE FLIGHT CONTROL SYSTEM; COMPUTATIONAL BURDEN; LINEAR QUADRATIC REGULATOR; RECONFIGURABLE CONTROL; RECONFIGURABLE CONTROL SYSTEMS; SCHEDULING PARAMETERS; STABILITY ANALYSIS METHOD; TIME VARYING PARAMETER;

CONTROL SYSTEM STABILITY;

EID: 84959091871     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4111     Document Type: Conference Paper

References (9)

1. J. S. Brinker and K. A. Wise, "Reconfigurable Flight Control for a Tailless Advanced Fighter Aircraft", Proc. Of the 1998 AIAA GNC Conference.
2. ∞ Control", Int. Journal of Robust and Nonlinear Control, Vol. 4, pp. 421-448, 1994.
3. Wu, Fen, X. H. Yang, A. Packard, and G. Becker, "Induced L2-Norm Control for LPV System with Bounded Parameter Variation Rates", Int. Journal of Robust and Nonlinear Control, Vol. 4, 1994.
4. S. Boyd, L. El Ghaoui, E. Feron, and V. Balakrishnan, Linear Matrix Inequalities in System and Control Theory, SIAM, Philadelphia PA, 1994.
5. G. Becker, A. Packard, D. Philbrick, and G. Balas, "Control of Parametrically-Dependent Linear Systems: A Single Quadratic Lyapunov Approach", Proc. of the ACC, San Francisco CA, June 1993, pp. 2795-2799.
6. G. Becker and A. Packard, "Gain-Scheduled State-Feedback with Quadratic Stability for Uncertain Systems", IEEE CDC, pp. 2702-2703.
7. J. Doyle, A. Packard, K. Zhou, "Review of LFTs, LMIs, and μ", Proc. of the IEEE CDC, Brighton England, Dec. 1991, pp. 1227-1232.
8. K. A. Wise, "Bank-to-Turn Missile Autopilot Design Using Loop Transfer Recovery", AIAA Journal of Guidance, Control, and Dynamics, Vol. 13, No. 1, Jan-Feb. 1990, pp. 145-152.
9. K. A. Wise and F. Deylami, "Approximating a Linear Quadratic Missile Autopilot Design Using an Output Feedback Projective Control", Proc. of the AIAA Guidance, Navigation, and Control Conference, New Orleans, LA, Aug. 1991, p 114-122, AIAA Paper No. 91-2613.