Systematic gain-scheduling control design: A missile autopilot example

Asian Journal of Control

Volumn 4, Issue 3, 2002, Pages 341-347

  Wu, Fen ^a   Packard, Andy ^b   Balas, Gary ^c  

^a North Carolina State University   (United States)

^b UNIVERSITY OF CALIFORNIA   (United States)

^c University of Minnesota   (United States)

Author keywords

Control design; Gain scheduling control; Linear parameter varying system; Missile autopilot

Indexed keywords

AUTOMATIC PILOTS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; GAIN CONTROL; LINEAR SYSTEMS; MATHEMATICAL MODELS; SCHEDULING; SYSTEM STABILITY;

GAIN SCHEDULING CONTROL; LINEAR PARAMETER VARYING SYSTEMS; MISSILE AUTOPILOTS;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0036760092     PISSN: 15618625     EISSN: None     Source Type: Journal    
DOI: 10.1111/j.1934-6093.2002.tb00362.x     Document Type: Article

References (21)

1. Apkarian, P., On the Discretization of LMI-Synthesized Linear Parameter-Varying Controllers, Automatica, Vol.33, No.4, pp. 655-661 (1997).
2. Apkarian, P. and R.J. Adams, Advanced Gain-Scheduling Techniques for Uncertain System, IEEE Trans. Contr. Syst. Technol., Vol.6, No.1, pp. 21-32 (1998).
3. ∞ Controllers, IEEE Trans. Automat. Contr., Vol.40, No.9, pp. 853-864 (1995).
4. ∞ Control of Linear Parameter-Varying Systems: A Design Example, Automatica, Vol.31, No.9, pp. 1251-1261 (1995).
5. st IEEE Conf. Contr. Appl., Dayton, OH. (1992).
6. Becker, G. and A. Packard, Robust Performance of Linear Parametrically Varying Systems using Parametrically Dependent Linear Dynamic Feedback, Syst. Contr. Letts., Vol. 23, No.3, pp. 205-215. (1994).
7. Bennani, S., D.M.C. Willemsen, and C.W. Scherer, Robust LPV Control with Bounded Rates, in Proc. AIAA Guidance Nav. Contr. Conf., New Orleans, LA (1997).
8. Boyd, S., L. El Ghaoui, E. Feron, and V. Balakrishnan, Linear Matrix Inequalities in Systems and Control Theory, SIAM (1993).
9. Gahinet, P., A. Nemirovskii, A. Laub and M. Chilali, LMI Control Toolbox, Mathworks, Natick, MA (1995).
10. 2-Gain Synthesis on LPV Missile Autopilot Design, in Proc. Amer. Contr. Conf., pp. 3733-3737, San Diego, CA (1999).
11. Nichols, R.A., R.T. Reichert and W.J. Rugh, Gain Scheduling for H-infinity Controllers: A Flight Control Example, IEEE Trans. Contr. Syst. Technol., Vol.1, No.2, pp. 69-79 (1993).
12. Packard, A., Gain Scheduling via Linear Fractional Transformations, Syst. Contr. Letts., Vol.22, pp. 79-92 (1994).
13. Reichert, R.T., Robust Autopilot Design Using μ-synthesis, in Proc. Amer. Contr. Conf., pp. 2368-2373, San Diego, CA (1990).
14. Reichert, R.T., Dynamic Scheduling of Modern-Robust-Control Autopilot Designs for Missiles, IEEE Contr. Syst. Mag., Vol.12, No.5, pp. 35-42 (1992).
15. Rugh, W.J., Analytical Framework for Gain Scheduling, IEEE Contr. Syst. Mag., Vol.11, pp. 74-84 (1991).
16. Rugh, W.J. and J.S. Shamma, Research on Gain Scheduling, Automatica, Vol.36, pp. 1401-1425 (2000)
17. Shamma, J.S. and M. Athans, Guaranteed Properties of Gain Scheduled Control for Linear Parameter varying Plants, Automatica, Vol.27, No.3, pp. 559-564 (1991).
18. Shamma, J.S. and J.R. Cloutier, Gain-Scheduled Missile Autopilot Design using Linear Parameter Varying Transformations, J. Guidance Contr. Dyn., Vol. 16, No.2, pp. 256-263 (1993).
19. Wu, F., Control of Linea Parameter Varying Systems, Ph.D. Dissertation, University of California, Berkeley, CA (1995).
20. th IEEE Conf. Dec. Contr., pp. 188-193, New Orleans, LA (1995).
21. 2 Norm Control for LPV Systems with Bounded Parameter Variation Rates, Int. J. Robust Nonlin. Contr., Vol.6, No.9/10, pp. 983-998 (1996).