Receding horizon guidance laws with no information on the time-to-go

Journal of Guidance, Control, and Dynamics

Volumn 23, Issue 2, 2000, Pages 193-199

  Kim, Ki Baek ^a   Kim, Myung Joon ^a   Kwon, Wook Hyun ^a  

^a Seoul National University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; ELECTRONIC GUIDANCE SYSTEMS;

MISS DISTANCE (MD) RATE; RECEDING HORIZON GUIDANCE LAW (RHG);

OPTIMAL CONTROL SYSTEMS;

EID: 0033870946     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4518     Document Type: Article

References (15)

1. Nesline, F. W., and Zarchan, P., "A New Look at Classical vs Modern Homing Missile Guidance," Journal of Guidance and Control, Vol. 4, No. 1, 1979, pp. 78-85.
2. Ha, I. J., Hur, J. S., Ko, M. S., and Song, T. L., "Performance Analysis of PNG Laws for Randomly Maneuvering Targets," IEEE Transactions on Aerospace and Electronic Systems, Vol. 26, No. 5, 1990, pp. 713-721.
3. Holder, E. J., and Sylveser, V. B., "An Analysis of Modern Versus Classical Homing Guidance," IEEE Transactions on Aerospace and Electronic Systems, Vol. 26, No. 4, 1990, pp. 599-606.
4. Garber, V., "Optimum Intercept Laws for Accelerating Targets," AIAA Journal, Vol. 6, No. 11, 1968, pp. 2196-2198.
5. Cottrell, R. G., "Optimal Intercept Guidance for Short-Range Tactical Missiles," AIAA Journal, Vol. 9, No. 7, 1971, pp. 1414, 1415.
6. Asher, R. B., and Matuszewski, J. P., "Optimal Guidance with Maneuvering Targets," Journal of Spacecraft and Rockets, Vol. 11, No. 3, 1974, pp. 204-206.
7. Nazaroff, G. J., "An Optimal Terminal Guidance Law," IEEE Transaction on Automatic Control, Vol. 21, No. 6, 1976, pp. 407, 408.
8. Rusnak, I., and Meir, L., "Optimal Guidance for High-Order and Acceleration Constrained Missile," Journal of Guidance, Control, and Dynamics, Vol. 14, No. 3, 1991, pp. 589-596.
9. Cho, H., and Ryoo, C. K., "Closed-Form Optimal Guidance Law for Missiles of Time-Varying Velocity," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 5, 1996, pp. 1017-1022.
10. Lee, G. K. F., "Estimation of the Time-to-Go Parameter for Air-to-Air Missiles," Journal of Guidance, Control, and Dynamics, Vol. 8, No. 2, 1985, pp. 262-266.
11. Lin, C. F., Modern Navigation, Guidance, and Control Processing, Prentice-Hall, Upper Saddle River, NJ, 1991, pp. 35-37.
12. Hull, D. G., Radke, J. J., and Mack, R. E., "Time-to-Go Prediction for Homing Missiles Based on Minimum-Time Intercepts," Journal of Guidance, Control, and Dynamics, Vol. 14, No. 5, 1991, pp. 865-871.
13. Kwon, W. H., and Pearson, A. E., "A Modified Quadratic Cost Problem and Feedback Stabilization of a Linear System," IEEE Transaction on Automatic Control, Vol. 22, No. 5, 1977, pp. 838-842.
14. ∞ Tracking Control for Discrete Linear Periodic Systems," IEEE Transaction on Automatic Control (to be published).
15. Garcia, C. E., Prett, D. M., and Morari, M., "Model Predictive Control: Theory and Practive - A Survey," Automatica, Vol. 25, No. 3, 1989, pp. 335-348.