Impact-angle-constrained suboptimal model predictive static programming guidance of air-to-ground missiles

Journal of Guidance, Control, and Dynamics

Volumn 35, Issue 1, 2012, Pages 153-164

  Oza, Harshal B ^a,b,c   Padhi, Radhakant ^a,b  

^a INDIAN INSTITUTE OF SCIENCE   (India)

^b Department of Aerospace Engineering ^*  (India)

^c UNIVERSITY OF KENT   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; AIR TO SURFACE MISSILES; AMMUNITION; ELECTRONIC GUIDANCE SYSTEMS;

AIR TO GROUND MISSILE; AUGMENTED PROPORTIONAL NAVIGATION; IMPACT ANGLE CONSTRAINTS; INACCURATE INFORMATION; NONLINEAR ENGAGEMENTS; SUBOPTIMAL GUIDANCE LAW; TERMINAL IMPACT ANGLES; THREEDIMENSIONAL (3-D);

GUIDED MISSILES;

EID: 84855315718     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.53647     Document Type: Article

References (26)

1. Zarchan, P., Tactical and Strategic Missile Guidance, Progress in Astronautics and Aeronautics Series, AIAA, 5th ed., 2007
2. Siouris, G. M., Missile Guidance and Control Systems, Springer, New York, 2003
3. Kim, B. S., Lee, J. G., and Han, S. H., "BiasedPNGLaw for Impact with Angular Constraint," IEEE Transactions on Aerospace and Electronic Systems, Vol. 34, No. 1, 1998, pp. 277-288. doi:10.1109/7.640285
4. Ryoo, C.-K., Cho, H., and Tahk, M.-J., "Optimal Guidance Laws with Terminal Impact Angle Constraint," Journal of Guidance, Control, and Dynamics, Vol. 28, No. 4, July-Aug. 2005, pp. 724-732. doi:10.2514/1.8392 (Pubitemid 41049815)
5. Kim, M., and Grider, K., "Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories," IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-9, No. 6, Nov. 1973, pp. 852-859. doi:10.1109/TAES.1973.309659
6. Ryoo, C. K., and Cho, H., "Optimal Guidance with Terminal Impact Angle and Control Constraint," Proceedings of the Proceedings of the 1992 Korean Automatic Control Conference, Korean Automatic Control Council, Seoul, Republic of Korea, 1992, pp. 601-606, (in Korean).
7. Ben-Asher, J., and Yaesh, I., Advances in Missile Guidance Theory, Progress in Astronautics and Aeronautics Series, Vol. 180, AIAA, Reston, VA, 1998.
8. Song, T., Shin, S., and Cho, H., "Impact angle control for planar engagements," IEEE Transactions on Aerospace and Electronic Systems, Vol. 35, No. 4, Oct. 1999, pp. 1439-1444. doi:10.1109/7.805460 (Pubitemid 30546593)
9. Shaferman, V., and Shima, T., "Linear Quadratic Guidance Laws for Imposing a Terminal Intercept Angle," Journal of Guidance, Control, and Dynamics, Vol. 31, No. 5, Oct. 2008, pp. 1400-1412. doi:10.2514/1.32836
10. Ratnoo, A., and Ghose, D., "SDRE Based Guidance Law for Impact Angle Constrained Trajectories," Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA, Hilton Head, SC, 20-23 Aug. 2007.
11. Ratnoo, A., and Ghose, D., "Impact Angle Constrained Interception of Stationary Targets," Journal of Guidance, Control, and Dynamics, Vol. 31, No. 6, Nov.-Dec. 2008, pp. 1817-1822. doi:10.2514/1.37864
12. Shima, T., "Deviated Velocity Pursuit," Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA, Hilton Head, SC, 20-23 Aug. 2007
13. Lee, J.-I., Jeon, I.-S., andTahk, M.-J., "Guidance Law to Control Impact Time and Angle," IEEE Transactions on Aerospace and Electronic Systems, Vol. 43, No. 1, Jan. 2007, pp. 301-310. doi:10.1109/TAES.2007.357135 (Pubitemid 46773723)
14. Harl, N., and Balakrishnan, S., "Impact Time and Angle Guidance with Sliding Mode Control," Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Chicago, IL, 10-13 Aug. 2009.
15. Weimeng, S., and Zhiqiang, Z., "3-D Variable Structure Guidance Law Based on Adaptive Model-Following Control with Impact Angular Constraints," Proceedings of the Chinese Control Conference, IEEE, July 2007, pp. 61-66.
16. Gu, W.-J., Yu, J.-Y., and Zhang, R.-C., "A 3-D Missile Guidance Law with Angle Constraint Based on Sliding Mode Control," IEEE International Conference on Control and Automation, IEEE, Angers, France, May 2007, pp. 299-302.doi:10.1109/ICCA.2007.4376367
17. Ohlmeyer, E. J., and Phillips, C. A., "Generalized Vector Explicit Guidance," Journal of Guidance, Control, and Dynamics, Vol. 29, No. 2, Mar.-Apr. 2006, pp. 261-268. doi:10.2514/1.14956
18. Lukacs, J. A., and Yakimenko, O. A., "Trajectory-Shape-Varying Missile Guidance for Interception of Ballistic Missiles During the Boost Phase," Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA, Hilton Head, SC, 20-23 Aug. 2007.
19. Padhi, R., and Kothari, M., "Model Predictive Static Programming: A Computationally Efficient Technique for Suboptimal Control Design," International Journal of Innovative Computing, Information, and Control, Vol. 5, No. 2, Feb. 2009, pp. 399-411.
20. Chawla, C., Sarmah, P., and Padhi, R., "Suboptimal Reentry Guidance of Reusable Launch Vehicles Using Pitch Plane Maneuver," Aerospace Science and Technology, Vol. 14, No. 6, 2010, pp. 377-386. doi:10.1016/j.ast.2010.04.001
21. Dwivedi, P. N., Bhattacharya, A., and Padhi, R., "Suboptimal Midcourse Guidance of Interceptors for High Speed Targets with Alignment Angle Constraint," Journal of Guidance, Control, and Dynamics, Vol. 34, No. 3, 2011, pp. 860-877. doi:10.2514/1.50821
22. Bryson, A. E., and Ho, Y.-C., Applied Optimal Control, Wiley, New York, 1975.
23. Imado, F., Kuroda, T., and Tahk, M.-J., "A New Missile Guidance Algorithm Against a Maneuvering Target," Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA, Boston, MA, 10-12 Aug. 1998.
24. McHenry, R. L., Long, A. D., Cockrell, B., Thibodeau, J., and Brand, T. J., "Space Shuttle Ascent Guidance, Navigation, and Control," Journal of the Astronautical Sciences, Vol. 27, No. 1, 1979, pp. 1-38. (Pubitemid 9445347)
25. Gopal, M., Modern Control System Theory, 2nd ed.,Wiley, New York, 1993.
26. Shampine, L. F., Numerical Solution of Ordinary Differential Equations, Chapman & Hall, New York, 1994.