Integrated guidance and control for homing missiles

Johns Hopkins APL Technical Digest (Applied Physics Laboratory)

Volumn 25, Issue 2, 2004, Pages 121-138

  Palumbo, Neil F ^a,b   Reardon, Brian E ^a   Blauwkamp, Ross A ^c  

^a HoneywelI Aerosp Electronic Systems   (United States)

^b Johns Hopkins University   (United States)

^c Guid Navig and Contr Grp at APL ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FRAMEWORK; HOMING MISSILES; INTEGRATED GUIDANCE; INTERCEPTORS;

AIRCRAFT PROPULSION; ALGORITHMS; COMPUTER SIMULATION; CONTROL SYSTEMS; ELECTRONIC GUIDANCE SYSTEMS; FLIGHT DYNAMICS; OPTIMIZATION; PARAMETER ESTIMATION; SENSORS;

MISSILES;

EID: 16244377748     PISSN: 02705214     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (29)

1. Witte, R. W., and McDonald, R. L. "Standard Missile: Guidance System Development," Johns Hoplins APL Tech. Djg. 2(4), 289-298 (1981).
2. Bar-Shalom, Y., Li, X. R., and Kirubarajan, T., Estimation with Applications to Tracking and Navigation, Wiley and Sons Publishers (2001).
3. Grewal, M. S., and Andrews, A. P., Kalman Filtering Theory and Practice, Prentice Hall (1993).
4. Ben-Asher, J. Z., and Yaesh, I., Advance: m Missile Guidance Theory, American Institute of Aeronautics and Astronautics, Inc. (1998).
5. Shneydor, N. A., Missile Guidance and Pursuit: Kinematics, Dynamics and Control, Horwood Publishing (1998).
6. Locke, A. S., Princes of Guided Missile Design, D. Van Nostrand Company, Inc. (1955).
7. Schumacher, C., and Khargonekar, P. P., "Stability Analysts of a Missile Control System with a Dynamic Inversion Controller," J. Quid. Control Dyn. 21(3) (May-Jun 1998).
8. Etkin, B., Dynamics of Atmospheric Flight, Wiley and Sons (1972).
9. Basar, T., and Bernhard, P., H-Infinity Optimal Control and Related Minimax Design Problems, Birkhauser, Boston, MA (1995).
10. Bryson, A. E., and Ho, Y-C., Allied Optimal Control, Hemisphere Publishing Corporation (1975).
11. Rhee, I., and Speyer, J. L., "A Game Theoretic Approach to a Finite-Time Disturbance Attenuation Problem," IEEE Tram. Autom. Control 36(9), 1021-1032 (Sep 1991).
12. Cloutier, J. R., D'Souza, N., and Mracek, C. P., "Nonlinear Regulation and Nonlinear H-Infinity Control via the State-Dependent Riccati Equation Technique: Pans 1&2," in Proc. First Int. Conf., on Nonlinear Problems in Aviation and Aerospace, pp. 117-141 (9-11 May 1996).
13. Cloutier, J. R., Mracek, C. P., Ridgely, D. B., and Hammert, K. D., State Dependent Riccati Equation Techniques: Theory and Applications," ACC Workshop Tutorial #6 (1998).
14. Lin, C. F., Wang, Q., Speyer, J. L., Evers, J. H., and Cloutier, J. R., "Integrated Estimation, Guidance, and Control System Design Using Game Theoretic Approach," in Proc. Am. Control Conf., pp. 3220-3224 (1992).
15. Lin, C. F., Ohlmeyer, E., Bibel, J. E., and Malyevac, S., "Optimal Design of Integrated Missile Guidance and Control," World Aviation Conf., AIAA-985519 (Sep 1998).
16. Menon, P. K., Ohlmeyer, E. J., et al., "Integrated Design of Agile Missile Guidance and Control Systems," AIAA Missile Sciences Conf., Monterey, CA (Nov 1998).
17. O'Connell, J., Stability of the Epic Autopilot, ND-E-MIS-T-2151, RCA (Oct 1982).
18. Palumbo, N. F., A Fully Integrated Guidance and Control System for the Highly Responsive Missile Control System: Advanced Technology Demon-stration: Preliminary Development and Results, A1E(96)U-5-196, JHU/APL, Laurel, MD (7 Oct 1996).
19. Palumbo, N. F., and Casper, S. G., "Integration of a Missile Autopilot, Guidance Filter and Guidance Law," AIAA/BMDO Technology Conf. (Jul 2000).
20. Pearson, J. D., "Approximation Methods in Optimal Control," J. Electron. Control 13, 453-469 (1962).
21. Hammett, K. D., Control of Nonlmear Systems via State feedback State-Dependent Riccati Equation Techniques, Ph.D. Dissertation, AFIT (Jun 1997).
22. Rugh, W. J., and Shamma, J. S., "Research on Gain Scheduling," Automotica 36, 1401-1425 (2000).
23. Franklin, G. F., Powel, J. D., and Workman, M. L., Digital Control of Dynamic Systems, Addison-Wesley Publishers (Jun 1990).
24. Vaughan, D. R., "A Negative Exponential Solution for the Matrix Riccati Equation," IEEE Trans. Autom. Control 14(2), 72-75 (Feb 1969).
25. Vaughan, D. R., "A Kontecursive Algebraic Solution for the Discrete Riccati Equation," IEEE Trans. Autom. Control 15(10), 597-599 (Oct 1970).
26. Reardon, B. E., Palumbo, N. F., and Casper, S. G., "Simulation-Based Performance Optimization of Missile Guidance and Control Algorithms," AIAA/MDA 2002 Technol. Conf. (22-25 Aug 2002).
27. Spall, J. C., "Multivariate Stochastic Approximation Using a Simultaneous Perturbation Gradient Approximation," IEEE Trans. Autom. Control 37(3), 332-341 (Mar 1992).
28. Spall, J. C., "Implementation of Simultaneous Perturbation Algorithm for Stochastic Optimization," IEEE Trans. Aerosp. Electron. Sys. 34(3), 817-823 (Jul 1998).
29. Spall, J. C., "An Overview of the Simultaneous Perturbation Method for Efficient Optimistion," Johns Hopkins APL Tech. Dig. 19, 482-492 (1998).