Optimal planar evasive aircraft maneuvers against proportional navigation missiles

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 6, 1996, Pages 1210-1215

  Ong, Shaw Y ^a,c   Pierson, Bion L ^b,c  

^a Advanced System Department   (Singapore)

^b Iowa State University   (United States)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; COMPUTER SIMULATION; EQUATIONS OF MOTION; FLIGHT DYNAMICS; MANEUVERABILITY; MATHEMATICAL MODELS; MATHEMATICAL PROGRAMMING; MISSILES; NUMERICAL METHODS; OPTIMAL CONTROL SYSTEMS; OPTIMIZATION; SUPERSONIC AIRCRAFT;

MISSILE DYNAMICS; NAVIGATION MISSILES; PLANAR EVASIVE AIRCRAFT MANEUVERS; SEQUENTIAL QUADRATIC PROGRAMMING;

FIGHTER AIRCRAFT;

EID: 0030289222     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21773     Document Type: Article

References (18)

1. Vincent, T. L., Sticht, D. J., and Peng, W. Y., "Aircraft Missile Avoidance," Operations Research, Vol. 24, No. 3, 1976, pp. 420-437.
2. Julich, P. M., and Borg, D. A., "Proportional Navigation vs an Optimally Evading Constant-Speed Target in Two Dimensions," Journal of Spacecraft and Rockets, Vol. 7, No. 12, 1970, pp. 1454-1457.
3. Slater, G. L., and Wells, W. R., "Optimal Evasive Tactics with Time Delay," Journal of Spacecraft and Rockets, Vol. 10, No. 5, 1973, pp. 309-313.
4. Shinar, J., and Steinberg, D., "Analysis of Optimal Evasive Maneuvers Based on a Linearized Two-Dimensional Model," Journal of Aircraft, Vol. 14, No. 8, 1977, pp. 795-802.
5. Shinar, J., Rosenzstein, Y., and Bezner, E., "Analysis of Three-Dimensional Optimal Evasion with Linearized Kinematics," Journal of Guidance and Control, Vol. 2, No. 5, 1979, pp. 353-360.
6. Ben-Asher, J., Cliff, E. M., and Kelley, H. J., "Optimal Evasion with a Path-Angle Constraint and Against Two Pursuers," Journal of Guidance, Control, and Dynamics, Vol. 11, No. 4, 1988, pp. 300-304.
7. Ben-Asher, J., and Cliff, E. M., "Optimal Evasion Against a Proportionally Guided Pursuer," Journal of Guidance, Control, and Dynamics, Vol. 12, No. 4, 1989, pp. 598-600.
8. Forte, I., Steinberg, A., and Shinar, J., "Effects of Non-Linear Kinematics in Optimal Evasion," Optimal Control Applications and Methods, Vol. 4, No. 2, 1983, pp. 139-152.
9. Guelman, M., and Shinar, J., "Optimal Guidance Law in the Plane," Journal of Guidance, Control, and Dynamics, Vol. 7, No. 4, 1984, pp. 471-476.
10. Imado, F., and Miwa, S., "Fighter Evasive Maneuvers Against Proportional Navigation Missile," Journal of Aircraft, Vol. 23, No. 11, 1986, pp. 825-830.
11. Murtaugh, S. A., and Criel, H. E., "Fundamentals of Proportional Navigation," Spectrum, Vol. 3, No. 12, 1966, pp. 75-85.
12. Zarchan, P., Tactical and Strategic Missile Guidance, AIAA, Washington, DC, 1990, Chap. 2.
13. Miele, A., Flight Mechanics, Vol. 1: Theory of Flight Paths, Addison-Wesley, Reading, MA, 1962, Chap. 4.
14. Bryson, A. E., Jr., Desai, M. N., and Hoffmann, W. C., "Energy-State Approximation in Performance Optimization of Supersonic Aircraft," Journal of Aircraft, Vol. 6, No. 6, 1969, pp. 481-488.
15. Pierson, B. L., "Sequential Quadratic Programming and Its Use in Optimal Control Comparisons," Optimal Control Theory and Economic Analysis 3, edited by G. Feichtinger, North-Holland, Amsterdam, 1988, pp. 175-193.
16. Pierson, B. L., and Ong, S. Y., "Minimum-Fuel Aircraft Transition Trajectories," Mathematical and Computer Modelling, Vol. 12, No. 8, 1989, pp. 925-934.
17. Pouliot, M. R., "CONOPT2: A Rapidly Convergent Constrained Trajectory Optimization Program for TRAJEX," General Dynamics, Convair Div., Rept. GDC-SP-82-008, San Diego, CA, 1982.
18. Ong, S. Y., "A Model Comparison of a Supersonic Aircraft Minimum Time-to-Climb Problem," M.S. Thesis, Dept. of Aerospace Engineering, Iowa State Univ., Ames, IA, May 1986.