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Tactical Missile Guidance Laws

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Missile Guidance and Control Systems

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References

  1. Becker, K.: Closed-Form Solution of Pure Proportional Navigation, IEEE Transactions on Aerospace and Electronic Systems, Vol. 26,No. 3, May 1990, pp. 526–533.

    Article  Google Scholar 

  2. Blakelock, J.H.: Automatic Control of Aircraft and Missiles, John Wiley & Sons, Inc., New York, NY, second edition, 1991.

    Google Scholar 

  3. Bryson, A.E. Jr. and Ho, Y.C.: Applied Optimal Control, Revised Printing, Hemisphere Publishing Corporation, A Halsted Press Book, Washington, D.C., 1975.

    Google Scholar 

  4. Chui, C.K. and Chen G.: Kalman Filtering with Real-Time Applications, third edition, Springer-Verlag, Berlin, New York, NY, 1999.

    Google Scholar 

  5. Garber, V.: Optimum Intercept Laws for Accelerating Targets, AIAA Journal, Vol. 6,No. 11, November 1968.

    Google Scholar 

  6. Garnell, P.: Guided Weapon Control Systems, second edition, Pergamon Press, Oxford, New York, NY, 1980.

    Google Scholar 

  7. Ghose, D.: On the Generalization of True Proportional Navigation, IEEE Transactions on Aerospace and Electronic Systems, Vol. 30,No. 2, pp. 545–555.

    Google Scholar 

  8. Guelman, M.: Proportional Navigation with a Maneuvering Target, IEEE Transactions on Aerospace and Electronic Systems, Vol. 8,No. 3, May 1972, pp. 364–371.

    Google Scholar 

  9. Guelman, M.: The Closed Form Solution of True Proportional Navigation, IEEE Transactions on Aerospace and Electronic Systems, Vol. 12,No. 4, July 1976, pp. 472–482.

    MathSciNet  Google Scholar 

  10. 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, September 1990, pp. 713–721.

    Article  Google Scholar 

  11. James, J.P.: Homing Guidance, A-62-1732.3-68, Aerospace Corporation, September 14, 1962.

    Google Scholar 

  12. Kim, B.S., Lee, J.G., and Han, H.S.: Biased PNG Law Impact with Angular Constraint, IEEE Transactions on Aerospace and Electronic Systems, Vol. 34,No. 1, January 1998, pp. 277–288.

    Article  Google Scholar 

  13. Kumar, R.R., Seywald, H., Cliff, E.M., and Kelley, H.T.: Three-Dimensional Air-to-Air Missile Trajectory Shaping, Journal of Guidance, Control, and Dynamics, Vol. 18,No. 3, May–June 1995, pp. 449–464.

    Google Scholar 

  14. Lauer, T.M. and Llanso, S.L.: Encyclopedia of Modern U.S. Military Weapons, edited by W.J. Boyne, Berkley Books, New York, NY, 1995.

    Google Scholar 

  15. Lee, R.G., Garland-Collins, T.K., Johnson, D.E., Archer, E., Sparkes, C., Moss, G.M., and Mowat, A.W.: Guided Weapons, third edition, Brassey’s London, Washington, 1998.

    Google Scholar 

  16. Lee, G.T. and Lee, J.G.: Improved Command to Line-of-Sight for Homing Guidance, IEEE Transactions on Aerospace and Electronic Systems, Vol. 31,No. 1, January 1995, pp. 506–510.

    Article  Google Scholar 

  17. Lin, C.F.: Modern Navigation, Guidance, and Control Processing, Vol. II, Prentice Hall, Englewood Cliffs, New Jersey, 1991.

    Google Scholar 

  18. Locke, A.S.: Guidance, D. Van Nostrand Company, Princeton, New Jersey, 1956.

    Google Scholar 

  19. Massoumnia, M.A.: Optimal Midcourse Guidance Law for Fixed-Interval Propulsive Maneuvers, Journal of Guidance, Control, and Dynamics, Vol. 18,No. 3, May–June 1995, pp. 465–470.

    Article  Google Scholar 

  20. Mehrotra, K. and Mahapatra, P.R.: A Jerk Model for Tracking Highly Maneuvering Targets, IEEE Transactions on Aerospace and Electronic Systems, Vol. 33,No. 4, October 1997, pp. 1094–1105.

    Article  Google Scholar 

  21. Oh, J.H. and Ha, I.J.: Capturability of the 3-Dimensional Pure PNG Laws, IEEE Transactions on Aerospace and Electronic Systems, Vol. 35,No. 2, April 1999, pp. 491–503.

    Article  Google Scholar 

  22. Shinar, J., Rotszein, Y., and Bezner, E.: Analysis of Three-Dimensional Optimal Evasion with Linearized Kinematics, Journal of Guidance and Control, September–October 1979, pp. 353–360.

    Google Scholar 

  23. Shukla, U.S. and Mahapatra, P.R.: A Generalized Linear Solution of Proportional Navigation, IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-24,No. 3, May 1988, pp. 231–238.

    Article  Google Scholar 

  24. Shukla, U.S. and Mahapatra, P.R.: Optimization of Biased Proportional Navigation, IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-25,No. 1, January 1989, pp. 73–80.

    Article  Google Scholar 

  25. Siouris, G. M.: An Engineering Approach to Optimal Control and Estimation Theory, John Wiley & Sons, Inc., New York, NY, 1996.

    Google Scholar 

  26. Siouris, G.M.: Comparison Between Proportional and Augmented Proportional Navigation, Nachrichtentechnische Zeitschrift (NTZ-Communications Journal), 27. Jahrgang, Heft 7, July 1974, pp. 278–280.

    Google Scholar 

  27. Siouris, G.M. and Leros, A.P.: Minimum-Time Intercept Guidance for Tactical Missiles, Journal of Control-Theory and Advanced Technology (C-TAT), Vol. 4,No. 2, published by the MITA Press, Tokyo, Japan, June 1988, pp. 251–263.

    Google Scholar 

  28. Song, T.L.: Target Adaptive Guidance for Passive Homing Missiles, IEEE Transactions on Aerospace and Electronic Systems, Vol. 33,No. 1, January 1997, pp. 312–315.

    Article  Google Scholar 

  29. Song, T.L. and Um, T.Y.: CLOS + IRTH Composite Guidance, IEEE Transactions on Aerospace and Electronic Systems, Vol. 33,No. 4, October 1997, pp. 1339–1344.

    Article  Google Scholar 

  30. Warren, R.S., Price, C.F., Gelb, A., and Vander Velde, W.E.: Direct Statistical Evaluation of Nonlinear Guidance Systems, AIAA Guidance and Control Conference, Key Biscayne, FL, August 20–22, 1973, AIAA Paper No.73-836.

    Google Scholar 

  31. Willems, G.: Optimal Controllers for Homing Missiles, Report No. RE-TR-68-15, U.S. Army Missile Command, Redstone Arsenal, Alabama, September 1968.

    Google Scholar 

  32. Yang, C.D. and Yang, C.C.: Analytical Solution of 3D Realistic True Proportional Navigation, Journal of Guidance, Control, and Dynamics, Vol. 19,No. 3, May–June 1996.

    Google Scholar 

  33. Yang, C.D., Yeh, F.B., and Chen, J.H.: The Closed Form Solution of Generalized Proportional Navigation, Journal of Guidance, Control and Dynamics, Vol. 10,No. 2, March–April 1987, pp. 216–218.

    Google Scholar 

  34. Yang, C.D., Yeh, F.B., and Hsiao, F.B.: Generalized Guidance Law for Homing Missiles, IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-25,No. 2, March 1989, pp. 197–212.

    Article  Google Scholar 

  35. Zarchan, P.: Tactical and Strategic Missile Guidance, third edition, Vol. 157, Progress in Astronautics and Aeronautics, American Institute of Aeronautics and Astronautics, Inc., Washington, D.C., 1998.

    Google Scholar 

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(2004). Tactical Missile Guidance Laws. In: Missile Guidance and Control Systems. Springer, New York, NY. https://doi.org/10.1007/0-387-21816-5_4

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  • DOI: https://doi.org/10.1007/0-387-21816-5_4

  • Publisher Name: Springer, New York, NY

  • Print ISBN: 978-0-387-00726-7

  • Online ISBN: 978-0-387-21816-8

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