Zero-miss-distance guidance law based on line-of-sight rate measurement only

Control Engineering Practice

Volumn 11, Issue 7, 2003, Pages 819-832

  Gurfil, Pini ^a  

^a Princeton University   (United States)

Author keywords

Estimation; Missile guidance; Monte Carlo simulations; Proportional navigation; ZMD

Indexed keywords

ACCELERATION; COMPUTER SIMULATION; KALMAN FILTERING; MONTE CARLO METHODS;

NAVIGATION GUIDANCE;

ROBUSTNESS (CONTROL SYSTEMS);

FLIGHT CONTROL SYSTEM; MISSILE;

EID: 0042303798     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(02)00208-3     Document Type: Article

References (24)

1. Bar-Shalom, Y. & Li, X. R. (1993). Estimation and tracking: Principles, techniques and software (pp. 339-370) Boston: Artech House.
2. Cottrel, R. G. (1971). Optimal intercept guidance for short range tactical missiles. AIAA Journal, 9, 1414-1415.
3. Creaser, P. A., Stacey, B. A., & White, B. A. (1998). Fuzzy missile guidance. Proceedings of AIAA conference, Boston, USA, 10-12 August 1998.
4. Fitzgerald, R. J. (1979). Shaping filters for disturbances with random starting times. Journal of Guidance and Control, 2(2), 152-154.
5. Gurfil, P., Jodorkovsky, M., & Guelman, M. (1998). Simple guidance law against highly maneuvering targets. In Proceedings of the 36th AlAA conference on guidance, navigation and control, Boston, MA, August 1998 (pp. 570-580).
6. Gurfil, P., Jodorkovsky, M., & Guelman, M. (2000). Design of nonsaturating guidance systems. Journal of Guidance, Control and Dynamics, 23(4), 693-700.
7. Gurfil, P., Jodorkovsky, M., & Guelman, M. (2001). Neoclassical guidance for homing missiles. Journal of Guidance, Control and Dynamics, 24(3), 452-459.
8. Gutman, S. (1979). On optimal guidance for homing missiles. Journal of Guidance, Control and Dynamics, 2(4), 296-300.
9. Hepner, S. A. R., & Geering, H. P. (1990). Observability analysis for target maneuver estimation via bearing-only and bearing-rate-only measurements. Journal of Guidance, Control, and Dynamics, 13(6), 977-983.
10. Holder, E. J., & Sylvester, V. B. (1990). An analysis of modern versus classical homing guidance. IEEE Transactions on Aerospace and Electronic Systems, 26(4), 599-605.
11. Kalman, R. E., & Bucy, R. S. (1961). New results in linear filtering and prediction theory. Transactions of the ASME, Journal of Basic Engineering, 83D, 95-108.
12. Nesline, F. W. & Nesline, M. L. (1984). Homing missile autopilot response sensitivity to stability derivative variations. In Proceedings of the 23rd IEEE conference on decision and control, Las Vegas, December 1984.
13. Ohlmeyer, E. J. (1996). Root-mean-square miss distance of proportional navigation missile against sinusoidal target. Journal of Guidance, Control, and Dynamics, 19(3), 563-568.
14. Rusnak, I., & Meir, L. (1991). Optimal guidance for high order and acceleration constrained missile. Journal of Guidance, Control, and Dynamics, 14(3), 589-596.
15. Shinar, J., Shima, T.. & Kebke. A. (1998). On the validity of linearized analysis in the interception of re-entry vehicles. In Proceeding of the 1998 AlAA guidance, navigation and control conference, Boston, MA, paper CP-4303.
16. Shinar, J.. & Steinberg, D. (1977). Analysis of optimal evasive maneuvers based on a linearized two-dimensional kinematic model. Journal of Aircraft, 14(8), 795-802.
17. Shneydor, N. A. (1998). Missile guidance and pursuit: Kinematics, dynamics and control. Harwood Publishing, Chapter 5, (pp. 125-148).
18. Singer, R. A. (1970). Estimating optimal tracking filter performance for manned maneuvering targets. IEEE Transactions on Aerospace and Electronic Systems, AES-6(4), 321-328.
19. Tang, Y. M. & Borrie, J. A. (1984). Missile guidance based on Kalman filter estimation of target maneuver. IEEE Transactions on Aerospace and Electronic Systems, AES-20(6).
20. Weiss, H. & Hexner, G. (1998). Modern guidance laws with model mismatch. In Proceedings of the IFAC symposium on missile guidance, Tel-Aviv, Israel, January 1998.
21. Zadeh, L. A. & Desoer, C. H. (1963). Linear system theory-the state space approach (pp. 337-369). New York: McGraw-Hill.
22. Zarchan, P. (1979). Complete statistical analysis of nonlinear missile guidance systems-SLAM. Journal of Guidance and Control, 2, 71-78.
23. Zarchan, P. (1995). Proportional navigation and weaving targets. Journal of Guidance, Control and Dynamics, 18(5), 969-974,
24. Zarchan, P. (1990). Tactical and strategic missile guidance, progress in aeronautics and astronautics, Vol. 124 (pp. 37-58). Washington, DO AIAA.