End-game guidance laws for dual-control missiles

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 219, Issue 2, 2005, Pages 157-170

  Shima, T ^a,b   Golan, O M ^a  

^a RAFAEL   (Israel)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Canard; Differential games; Guidance; Missile; Optimal control; Tail

Indexed keywords

ACOUSTIC NOISE MEASUREMENT; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; ELECTRONIC GUIDANCE SYSTEMS; FLIGHT DYNAMICS; GAME THEORY; MONTE CARLO METHODS; OPTIMAL CONTROL SYSTEMS; SENSITIVITY ANALYSIS;

CANARD; DIFFERENTIAL GAMES; GUIDANCE; OPTIMAL CONTROL; TAIL;

MISSILES;

EID: 21244432777     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/095441005X7249     Document Type: Conference Paper

References (20)

1. Gutman, S. The superiority of canards in homing missiles. IEEE Transactions on Aerospace and Electronic Systems, 2003, 39(3), 740-746.
2. Thukral, A. and Innocenti, M. A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering. IEEE Trans. Control Systems Technol., 1998, 6(3), 359-371.
3. Bhat, M. S., Bai, D. S., Powly, A. A., Swami, K. N., and Chose, D. Variable structure controller design with application to missile tracking. J. Guidance, Control, Dynamics, 2001, 24(4), 859-862.
4. Menon, P. K. and Iragavarapu, V. R. Adaptive techniques for multiple actuator blending. In Proceedings of the AIAA Guidance, Navigation, and Control Conference, Conference Publication CP-1998-4494, Boston, Massachusetts, 1998.
5. McFarland, M. B. and Calise, A. J. Adaptive nonlinear control of agile anti-air missiles using neural networks. IEEE Trans. Control Systems Technol., 2000, 8(5), 749-756.
6. Hirokawa, R., Sato, K., and Manabe, S. Autopilot design for a missile with reaction-jet using coefficient diagram method. In Proceedings of the AIAA Guidance, Navigation, and Control Conference, Conference Publication CP-2001-4162, Montreal, Canada, 2001.
7. Manabe, S. Application of coefficient diagram method to dual-control-surface missile. In Proceedings of the 15th IFAC Symposium on Automatic Control in Aerospace, Bologna, Italy, 2001, pp. 499-504.
8. Shima, T. and Golan, M. O. Linear quadratic guidance laws for a dual controlled missile. In Proceedings of the AIAA Guidance Navigation and Control Conference, Conference Publication CP-2002-4841, Monterey, California, 2002.
9. Shima, T. and Golan, M. O. Bounded differential game guidance law for a dual controlled missile. In Proceedings of the American Control Conference, Denver, Colorado, June 2003, pp. 390-395.
10. Friedland, B. Control System Design: An Introduction to State Space Methods, 1996, pp. 152-155 (McGraw-Hill, New York).
11. Cottrell, R. G. Optimal intercept guidance for shortrange tactical missiles. Am. Inst. Aeronaut. Astronaut. J., 1971, 9(7), 1414-1415.
12. Ben-Asher, J. and Yaesh, I. Advances in Missile Guidance Theory, Progress in Astronautics and Aeronautics, Vol. 180, 1998, pp. 89-126 (American Institute of Aeronautics and Astronautics Washington, DC).
13. Shinar, J. Solution techniques for realistic pursuit - evasion games, Advances in Control and Dynamic Systems, Vol. 17, 1981, pp. 63-124 (Academic Press, New York).
14. Singer, R. A. Estimating optimal tracking filter performance for manned maneuvering targets. IEEE Trans. Aerospace Electronic Systems, 1970, 6, 473-483.
15. Forte, I. and Shinar, J. Improved guidance law design based on mixed strategy concept. J. Guidance, Control Dynamics, 1989, 12(5), 739.
16. Wltsenhausen, H. S. Separation of estimation and control for discrete time systems. Proc. IEEE, November 1971, 59(11), 1557-1566.
17. Shinar, J. and Shima, T. Non-orthodox guidance law development approach for intercepting maneuvering targets. J. Guidance, Control, Dynamics, 2002, 25(4), 658-666.
18. Moon, J. and Kim, Y. Design of missile guidance law via variable structure control. In Proceedings of the AIAA Guidance Navigation and Control Conference, Denver, Colorado, 2000, paper 4068.
19. Shima, T., Idan, M., and Golan O. M. Sliding mode control for integrated missile autopilot-guidance. Presented at the AIAA Guidance Navigation and Control Conference, Providence, Rhode Island, August 2004.
20. Shkolnikov, I. A. and Shtessel, Y. B. Aircraft nonminimum phase control in dynamic sliding manifolds. J. Guidance Control Dynamics, 2001, 24(3), 566-572.