Two-step optimal estimator for three dimensional target tracking

IEEE Transactions on Aerospace and Electronic Systems

Volumn 41, Issue 3, 2005, Pages 780-793

  Gurfil, Pini ^a   Kasdin, N Jeremy ^b  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b Princeton University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMATIC TARGET RECOGNITION; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; ELECTRONIC GUIDANCE SYSTEMS; KALMAN FILTERING; MATHEMATICAL MODELS; PARAMETER ESTIMATION; RANDOM PROCESSES; TRACKING (POSITION); VECTORS;

EXTENDED KALMAN FILTER (EKF); FLIGHT CONTROL SYSTEM; OPTIMAL ESTIMATION ALGORITHM; TARGET TRACKING; THREE DIMENSIONAL TRACKING; TWO-STEP OPTIMAL ESTIMATOR (TSE);

STATE ESTIMATION;

EID: 27844554826     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2005.1541429     Document Type: Article

References (24)

1. Balakrishnan, S. N. Extension to modified polar coordinates and application with passive measurements. Journal of Guidance, Control and Dynamics, 12, 6 (Nov.-Dec. 1989), 906-912.
2. Stallard, D. V. Angle-only tracking filter in modified spherical coordinates. Journal of Guidance, Control and Dynamics, 14, 3 (May-June 1991), 694-696.
3. Vergez, P. L., and Randall, K. L. Target acceleration modeling for tactical missile guidance. Journal of Guidance, Control and Dynamics, 7, 3 (May-June 1984), 315-321.
4. Aidala, V. J., and Hammel, S. E. Utilization of modified polar coordinates for bearing-only tracking. IEEE Transactions on Automatic Control, AC-28, 3 (Mar. 1980), 283-294.
5. Balakrishnan, S. N., and Speyer, J. L. Coordinate-transformation-based filter for improved target tracking. Journal of Guidance, Control and Dynamics, 9 (Nov.-Dec. 1986), 704-709.
6. Aidala, V. J. Kalman filter behavior in bearings-only tracking applications. IEEE Transactions on Aerospace and Electronic Systems, AES-15, I (Jan. 1979), 29-39.
7. Tang, Y. M., and Borrie, J. A. Missile guidance based on Kalman filter estimation of target maneuver. IEEE Transactions on Aerospace and Electronic Systems, AES-20, 6 (Nov. 1984).
8. Hepner, S. A. R., and Geering, H. P. Observability analysis for target maneuver estimation via bearing-only and bearing-rate-only measurements. Journal of Guidance, Control, and Dynamics, 13, 6 (Nov.-Dec. 1990), 977-983.
9. Weiss, H., and Moore, J. B. Improved extended Kalman filter design for passive tracking. IEEE Transactions on Automatic Control, AC-25, 4 (Aug. 1980), 807-811.
10. Hepner, S. A. R., and Geering, H. P. Adaptive two-time-scale tracking filter for target acceleration estimation. Journal of Guidance, Control, and Dynamics, 14, 3 (May-June 1991), 581-588.
11. Chang, W. T., and Lin, S. A. Incremental maneuver estimation model for target tracking. IEEE Transactions on Aerospace and Electronic Systems, 28, 2 (Apr. 1992), 439-451.
12. Oshman, Y., and Shinar, J. Using a multiple model adaptive estimator in a random evasion missile/aircraft estimation. In Proceedings of the AIAA Guidance, Navigation and Control Conference, Portland, OR, Aug. 1999; AIAA Paper 99-4141.
13. Bar-Shalom, Y., and Li, X. R. Estimation and Tracking: Principles, Techniques and Software. Norwood, MA: Artech House, 1993, ch. 9, 625-655.
14. Saulson, B. Comparison of nonlinear estimation for ballistic missile tracking. Proceedings of SPIE - The International Society for Optical Engineering, 5096 (2003), 13-24.
15. Bergman, N., and Karlsson, R. Auxiliary particle filters for tracking a maneuvering target. In Proceedings of the IEEE Conference on Decision and Control, vol. 4, 2000, 3891-3895.
16. Haupt, G. T., Kasdin, N. J., Keiser, G. M., and Parkinson, B. W. An optimal recursive iterative algorithm for discrete nonlinear least-squares estimation. Journal of Guidance, Control, and Dynamics, 19, 3 (May-June 1996), 643-649.
17. Singer, R. A. Estimating optimal tracking filter performance for manned maneuvering targets. IEEE Transactions on Aerospace and Electronic Systems, AES-6, 4 (July 1970).
18. Fitzgerald, R. J. Shaping filters for disturbances with random starting times. Journal of Guidance and Control, 2, 2 (Mar.-Apr. 1979), 152-154.
19. Bryson, A. E., and Ho, Y. C. Applied Optimal Control. Washington, DC: Hemisphere Publishing, 1975.
20. Kasdin, N. J., and Haupt, G. T. Second-order correction and numerical considerations for the two-step optimal estimator. Journal of Guidance, Control, and Dynamics, 20, 2 (Mar.-Apr. 1997), 362-369.
21. Gelb, A. (Ed.) Applied Optimal Estimation. Cambridge, MA: The M.I.T. Press, 1974.
22. Stengel, R. F. Stochastic Optimal Control, Theory and Application. New York: Wiley, 1986.
23. Zarchan, P. Tactical and strategic missile guidance. Progress in Aeronautics and Astronautics, Vol. 124, Washington, DC: AIAA, 1990, ch. 3, 37-58.
24. Cottrel, R. G. Optimal intercept guidance for short range tactical missiles. AIAA Journal, 9 (July 1971), 1414-1415.