Nonlinear integrated guidance-control laws for homing missiles

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Menon, P K ^a   Ohlmeyer, Ernest J ^b  

^a OPTIMAL SYNTHESIS INC   (United States)

^b NAVAL SURFACE WARFARE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894433582     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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3. Menon, P. K., Dewell, L. D., and Sweriduk, G. D., "Integrated Guidance-Autopilot Designs for Anti-Jam Operation of Precision Munitions", Final Report prepared under Air Force Contract No. F08630-99-C- 0040, January 2000
4. Menon, P. K., and Iragavarapu, V. R., "Computer- Aided Design Tools for Integrated Flight/Propulsion Control System Synthesis", Final Report prepared under NASA Lewis Research Center Contract No. NAS3- 27578, June 1995.
5. Palumbo, N. F., and Jackson, T. D., "Integrated Missile Guidance and Control: A State Dependent Riccati Differential Equation Approach", 1999 IEEE International Conference on Control Applications, August 22-27, Kohala Coast, Hawai'i.
6. Ohlmeyer, E. J. (1996). "Root-Mean-Square Miss Distance of Proportional Navigation Missile Against Sinusoidal Target", Journal of Guidance, Control, and Dynamics, Vol. 19, May-June, pp. 563-568.
7. Zarchan, P., Tactical and Strategic Missile Guidance, AIAA Progress in Astronautics and Aeronautics, Vol. 176, Reston, VA, 1997.
8. Blakelock, J. H., Automatic Control of Aircraft and Missiles, John Wiley, New York, NY, 1965.
9. Isidori, A., Nonlinear Control Systems - An Introduction, Springer-Verlag, New York, 1989.
10. Slotine, J. J., and Li, W., Applied Nonlinear Control, Prentice-Hall, Englewood Cliffs, NJ, 1991.
11. Menon, P. K., et al, Nonlinear Synthesis Tools™ User's Manual, Optimal Synthesis Inc., Los Altos, CA, 2000.
12. Bryson, A. E., and Ho, Y. C., Applied Optimal Control, Hemisphere, New York, NY, 1975.
13. Wolovich, W. A. Automatic Control Systems, Harcourt-Brace, New York, NY, 1994.
14. Ohlmeyer, E. J., "Generalized Vector Explicit Guidance in Relative Missile-Target Coordinates", Private Communication, March 8, 2000.