Suboptimal midcourse guidance for inteception of free-fall targets

1999 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1999, Pages 672-679

  Song, Eun Jung ^a   Tahk, Min Jea ^a  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

MISSILES; REAL TIME CONTROL;

GUIDANCE LAWS; HORIZONTAL MOTION; MIDCOURSE GUIDANCE; ON-BOARD ALGORITHMS; OPTIMAL PERFORMANCE; REAL-TIME IMPLEMENTATIONS; THREE DIMENSIONAL SPACE; VERTICAL PLANE;

FEEDBACK LINEARIZATION;

EID: 84959156385     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Cheng, V. H. L. and Gupta, N. K., “Advanced midcourse guidance for air-to-air missiles,” Journal of Guidance, Control, and Dynamics, Vol. 9, No. 2, pp 135-142, 1986.
2. Menon, P. K. A. and Briggs, M. M., “Near-optimal midcourse guidance for air-to-air missiles,” Journal of Guidance, Control, and Dynamics, Vol. 13, No. 4, pp 596-602, 1990.
3. Dougherty, J. J. and Speyer, J. L., “Near-optimal guidance law for ballistic missile interception,” Journal of Guidance, Control, and Dynamics, Vol. 20, No. 2, pp 355-362, 1997.
4. Imado, F., Kuroda, T., and Miwa, S., “Optimal midcourse guidance for medium-range air-to-air missiles,” Journal of Guidance, Control, and Dynamics, Vol. 13, No. 4, pp 603-608, 1990.
5. Imado, F. and Kuroda, T., “Optimal midcourse guidance system against hypersonic targets,” Proc. of the AIAA Guidance and Control Conference, Hilton Head Island, SC, pp 1006-1011, 1992.
6. Newman, B., “Strategic intercept midcourse guidance using modified zero effort miss steering,” Journal of Guidance, Control, and Dynamics, Vol. 19, No. 1, pp 107-112, 1996.
7. Hornik, K., Stinchcombe, M., and White, H., “Multilayer feedforward networks are universal approximators,” Neural Networks, Vol. 2, pp 359-366, 1990.
8. Song, E. J., Lee, H., and Tahk, M. J., “On-line suboptimal midcourse guidance using neural networks,” Proc. of the 35th SICE Annual Conference, Tottori Univ., Japan, pp 1313-1318, 1996.
9. Khalil, H. K., Nonlinear Systems, Prentice-Hall, New Jersey, pp 81-85, 1996.
10. Siouris, G. M., Aerospace Avionics Systems: A Modem Synthesis, Academic Press, Inc., San Diego, California, 1993.
11. Song, E. J. and Tahk, M. J., “Real-time midcourse missile guidance robust to launch conditions,” to appear in Control Engineering Practice, 1999.
12. Regan, F. J. and Anandarkrishnan, S. M., Dynamics of Atmospheric Re-Entry, AIAA, Inc., Washington, DC, 1993.
13. Song, E. J. and Tahk, M. J., “Real-time midcourse guidance with intercept point prediction,” Control Engineering Practice, Vol. 6, No. 8, pp 957-967, 1998.
14. Hull, D. G., “Conversion of optimal control problems into parameter optimization problems,” Journal of Guidance, Control, and Dynamics, Vol. 20, No. 1, pp 5760, 1997.
15. Lawrence, C., Zhou, J. L., and Tits, A. L., User’s Guide for CFSQP Version 2-4: A C Code for Solving (Large Scale) Constrained Nonlinear (Minimax) Optimization Problems, Generating Iterates Satisfying All Inequality Constraints, University of Mayland, College Park, MD 20742, Institute for Systems Research TR-94-16rl, 1996.