Loop Shaping Design for Missile Autopilots: Controller Configurations and Weighting Filter Selection

Journal of Guidance, Control, and Dynamics

Volumn 23, Issue 3, 2000, Pages 516-525

  Iglesias, Pablo A ^a   Urban, Thomas J ^a  

^a JOHNS HOPKINS UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0005810697     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4558     Document Type: Article

References (25)

1. Fossier, M., "Development of Radar Homing Missiles," Journal of Guidance, Control, and Dynamics, Vol. 7, No. 6, 1984, pp. 641-651.
2. Stallard, D.,"Approach to Autopilot Design for Homing Interceptor Missiles," Proceedings of the Guidance, Navigation, and Control Conference, AIAA, Washington, DC, 1991, pp. 99-113.
3. McFarlane, D., and Glover, K., Robust Controller Design Using Normalized Coprime Factor Plant Descriptions, Springer-Verlag, Berlin, 1989.
4. ∞ Aerospace Control Design: VSTOL Flight Application, Springer-Verlag, London, 1995.
5. Walker, D., "Control of a Flexible Transmission - A Discrete Time H-Infinity Loop Shaping Approach," European Journal of Control, Vol. 1, No. 2, 1995, pp. 141-147.
6. Whidborne, J., Postlethwaite, I., and Gu, D., "Robust Control of a Paper Machine," Control Engineering Practice, Vol. 3, No. 10, 1995, pp. 1475-1478.
7. OBrien, R., Iglesias, P., and Urban, T., "Vehicle Lateral Control for Automated Highway Systems," IEEE Transactions on Control Systems Technology, Vol. 4, No. 3, 1996, pp. 266-273.
8. ∞ Design, Gap Metric and Real μ Analysis," AIAA Paper 96-3729, July 1996.
9. ∞ Loop Shaping and Partitioning," Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Reston, VA, 1998, pp. 989-998.
10. ∞ Controller for the NRC Bell 205 Experimental Fly-by-Wire Helicopter," Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Reston, VA, 1998, pp. 1023-1033.
11. ∞ Control into Flight," IEEE Conference on Decision and Control, Inst. of Electrical and Electronics Engineers, New York, 1993, pp. 1458-1463.
12. Pandiscio, A., and Mehta, A., "A Hybrid Classical/Modern Missile Autopilot Design Methodology," Missile Sciences Conf., Monterey, CA, Dec. 1998.
13. ∞ Loop Shaping Design Procedure," IEEE Conference on Control Applications, Inst. of Electrical and Electronics Engineers, New York, 1999, pp. 236-242.
14. Zames, G., "Feedback and Optimal Sensitivity: Model Reference Transformations, Multiplicative Seminorms, and Approximate Inverses," IEEE Transactions on Automatic Control, Vol. 26, No. 2, 1981, pp. 301-320.
15. Kasenally, E., and Limebeer, D., "Closed Formulae for a Parametric Mixed Sensitivity Problem," Systems and Control Letters. Vol. 12, No. 1, 1988, pp. 1-7.
16. ∞ Problem with Reference to a Two Block Design," Systems and Control Letters, Inst. of Electrical and Electronics Engineers, Piscataway, NJ, Vol. 14, No. 4, 1990, pp. 295-306.
17. ∞ Theory - A Design Example," IEEE Transactions on Automatic Control, Vol. 33, No. 5, 1988, pp. 477-479.
18. Doyle, J., and Stein, G., "Multivariable Feedback Design: Concepts for a Classical/Modern Synthesis," IEEE Transactions on Automatic Control, Vol. 26, No. 1, 1981, pp. 4-16.
19. Cronvich, L., "Aerodynamic Considerations for Autopilot Design," Tactical Missile Aerodynamics: General Topics, 2nd ed., edited by M. Hemsch, Vol. 141, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1992, pp. 29-68.
20. Nesling, F., and Nabbefeld, N., "Design of Digital Autopilots for Homing Missiles," Missile System Flight Dynamics, CP-270, AGARD, London, 1979, pp. 29-1-14.
21. Doyle, J., "Analysis of Feedback-Systems with Structured Uncertainties," IEE Proceedings. D. Control Theory and Applications, Vol. 129, No. 6, 1982, pp. 242-250.
22. Jackson, P., "Applying μ Synthesis to Missile Autopilot Design," IEEE Conference on Decision and Control, Inst. of Electrical and Electronics Engineers, New York, 1990, pp. 2993-2998.
23. Reichert, R., "Robust Autopilot Design Using μ-Synthesis," Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Washington, DC, 1990, pp. 2368-2373.
24. ∞ Optimal Control with μ Synthesis," Proceedings of the American Control Conference, IEEE, Piscataway, NJ, 1990, pp. 2362-2367.
25. ∞ Controllers to VSTOL Aircraft," IEEE Transactions on Automatic Control, Vol. 38, No. 7, 1993, pp. 1021-1039.