Dynamic inversion for missile lateral velocity control via polynomial eigenstructure assignment

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Bruyere L ^a   White, B A ^a   Tsourdos, A ^a  

^a CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; FLIGHT DYNAMICS; LINEAR SYSTEMS; MISSILES; POLYNOMIALS;

AERODYNAMIC DERIVATIVES; EXPLICIT DEPENDENCES; FAST RESPONSE TIME; LATERAL ACCELERATION; LATERAL VELOCITIES; POLYNOMIAL EIGENSTRUCTURE ASSIGNMENTS; TACTICAL MISSILES; TAIL-CONTROLLED MISSILES;

VERTICAL STABILIZERS;

EID: 85087192049     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5792     Document Type: Conference Paper

References (33)

1. Rugh, W. J., "Analytical Framework for Gain Scheduling," IEEE Control Systems Magazine, Vol. 11, 1993, pp. 799-803.
2. ∞ Controllers: A Flight Control Example," IEEE Transactions on Control Systems Technology, Vol. 1, 1993, pp. 69-79.
3. ∞ Controllers to a VSTOL Aircraft," IEEE Transactions on Automatic Control, Vol. 38, No. 7, 1993, pp. 1021-1039.
4. ∞ Control into Flight," 32nd IEEE Conference on Decision and Control, Vol. 2, 1993, pp. 1458-1463.
5. ∞ Control Law," Computing and Control Engineering Journal, Vol. 6, No. 1, 1995, pp. 11-16.
6. Baumann, W. T. and Rugh, W. J., "Feedback Control of Nonlinear Systems by Extended Linearization," IEEE Transactions on Automatic Control, Vol. 31, No. 1, 1986, pp. 40-46.
7. Wang, J. and Rugh, W. J., "Parameterized Linear Systems and Linearization Families for Nonlinear Systems," IEEE Transactions on Circuits and Systems, Vol. 34, No. 6, 1987, pp. 650-657.
8. Shamma, J. S. and Athans, M., "Analysis of Gain Scheduled Control for Nonlinear Plants," IEEE Transactions on Automatic Control, Vol. 35, No. 8, 1990, pp. 898-907.
9. Shamma, J. S. and Athans, M., "Guaranteed Properties of Gain Scheduled Control for Linear Parameter-Varying Plants," Automatica, Vol. 27, No. 3, 1991, pp. 559-564.
10. Shamma, J. S. and Athans, M., "Gain Scheduling: Potential Hazards and Possible Remedies," IEEE Control Systems Magazine, Vol. 13, 1992, pp. 101-107.
11. Shahruz, S. M. and Behtash, S., "Design of Controllers for Linear Parameter Varying Systems by the Gain Scheduling Technique," Journal of Mathematical Analysis and Applications, Vol. 168, No. 1, 1992, pp. 195-217.
12. Shamma, J. S. and Cloutier, J. R., "Gain-Scheduled Missile Autopilot Design Using LPV Transformations," Journal of Guidance, Control and Dynamics, Vol. 16, No. 2, 1993, pp. 256-263.
13. Balas, G. J., Doyle, J. C., Glover, K., Packard, A., and Smith, R., The μ-Analysis and Synthesis Toolbox, The MathWorks Inc., Cambridge, MA, 1994.
14. Packard, A. and Doyle, J. C., "The Complex Structured Singular Value," Automatica, Vol. 29, No. 1, 1993, pp. 71-109.
15. Packard, A., Doyle, J. C., and Balas, G., "Linear, Multivariable Robust Control with a μ-Perspective," Journal of Dynamic Systems, Measurement and Control, Vol. 115, No. 2B, 1993, pp. 426-438.
16. ∞ Control Problems," IEEE Transactions on Automatic Control, Vol. 34, No. 8, 1989, pp. 831-847.
17. ∞ Control," International Journal of Robust and Nonlinear Control, Vol. 4, No. 4, 1994, pp. 421-448.
18. ∞ Control State by State Feedback for Plants with Zeros on the Imaginary Axis," SIAM Journal on Control and Optimization, Vol. 30, No. 1, 1992, pp. 123-142.
19. ∞ Control Problem: A State Space Approach, Prentice-Hall, 1992.
20. ∞ Control of Linear Time-Varying Systems: A State Space Approach," SIAM Journal on Control and Optimization, Vol. 29, 1991, pp. 1394-1413.
21. Reboulet, C. and Champetier, C., "A New Method for Linearizing Nonlinear Systems: The Pseudolinearization," International Journal of Control, Vol. 40, No. 4, April 1984, pp. 631-638.
22. Lawrence, D. A. and Rugh, W. J., "Input-Output Pseudolinearization for Nonlinear Systems," IEEE Transactions on Automatic Control, Vol. 39, No. 11, November 1994, pp. 2207-2218.
23. Lawrence, D. A., "A Genereal Approach to Input-Output Pseudolinearization for Nonlinear Systems," IEEE Transactions on Automatic Control, Vol. 43, No. 10, October 1998, pp. 1497-1501.
24. Tsourdos, A., Zbikowski, R. and White, B. A., "Robust Design of Sideslip Velocity Autopilot for a Quasi-Linear Parameter-Varying Missile Model," Journal of Guidance, Control, and Dynamics, Vol. 24 of 2, American Institue of Aeronautics and Astronautics, 2001, pp. 287-295.
25. Bruyère, L., Tsourdos, A., Zbikowski, R., and White, B. A., "Robust performance study for lateral autopilot of a quasi-linear parameter-varying missile," American Control Conference, 2002, pp. 226-231.
26. Horton, M. P., A Study of Autopilots for the Adaptive Control of Tactical Guided Missiles, Master's thesis, University of Bath, 1992.
27. White, B. A., "Robust Polynomial Eigenstructure Assignment Using Dynamic Feedback Controllers," IMechE, Systems and Control Engineering, Vol. 211, No. I1, 1997, pp. 35-51.
28. White, B. A., "Flight Control of a VSTOL Aircraft Using Polynomial," IEE UKACC, International Conference on Control 96, Vol. 2, September 1996, pp. 758-763.
29. White, B. A., "Eigenstructure Assignment: A Survey," IMechE, Systems and Control Engineering, Vol. 209, No. I1, 1995, pp. 1-11.
30. Liu, G. and Patton, R., Eigenstructure Assignment for Control System Design, JohnWiley & Sons, Chichester, 1998.
31. Horton, M. P., "Autopilots for Tactical Missiles: An Overview," IMechE: Journal of Systems and Control Engineering, Vol. 209, 1995, pp. 127-139.
32. Wise, K. A., "Comparison of 6 Robustness Tests Evaluating Missile Autopilot Robustness to Uncertain Aerodynamics," Journal of Guidance, Control and Dynamics, Vol. 15, No. 4, 1992, pp. 861-870.
33. Horton, M. P., A Study of Autopilots for the Adaptive Control of Tactical Guided Missiles, Master's thesis, University of Bath, 1992.