High-order iterative learning identification of projectile's aerodynamic drag coefficient curve from radar measured velocity data

IEEE Transactions on Control Systems Technology

Volumn 6, Issue 4, 1998, Pages 563-570

  Chen, Yangquan ^a   Wen, Changyun ^b   Xu, Jian Xin ^a   Sun, Mingxuan ^c  

^a NATIONAL UNIVERSITY OF SINGAPORE   (Singapore)

^b NANYANG TECHNOLOGICAL UNIVERSITY   (Singapore)

^c XI'AN UNIVERSITY OF TECHNOLOGY   (China)

Author keywords

Aerodynamic drag coefficient; Curve identification; Data reduction; Iterative learning control; Minimax tracking; Optimal tracking control

Indexed keywords

CONTROL SYSTEM ANALYSIS; CURVE FITTING; DEGREES OF FREEDOM (MECHANICS); DRAG; IDENTIFICATION (CONTROL SYSTEMS); ITERATIVE METHODS; LEARNING SYSTEMS; MATHEMATICAL MODELS; OPTIMAL CONTROL SYSTEMS; POSITION CONTROL; PROJECTILES; TRACKING RADAR;

AERODYNAMIC DRAG COEFFICIENT; ITERATIVE LEARNING CONTROL; MINIMAX TRACKING; OPTIMAL TRACKING CONTROL;

TRACKING (POSITION);

EID: 0032124113     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.701354     Document Type: Article

References (18)

1. L. Ljung and S. T. Soderstrom, Theory and Practice of Recursive Identification. Cambridge, MA: MIT Press, 1983.
2. L. Ljung, System Identification. Englewood Cliffs, NJ: Prentice-Hall, 1987.
3. G. T. Chapman and D. B. Kirk, "A method for extracting aerodynamic coefficients from free flight data," AIAA J., vol. 18, no. 4, 1970.
4. R. F. Lieske and A. M. Mackenzie, "Determination of aerodynamic drag from radar data," Aberdeen Proving Ground Tech. Rep., 1972.
5. W. E. Williamson, Jr., "Instrument modeling for aerodynamic coefficient identification from flight test data," AIAA J. Guidance and Contr., vol. 3, no. 3, pp. 225-279, 1980.
6. C. Fratter and R. F. Stengel, "Identification of aerodynamic coefficients using flight testing data," AIAA Paper 83-2099, 1983.
7. K. W. Illif, "Parameter estimation for flight vehicle," AIAA J. Guidance and Contr., vol. 12, no. 5, pp. 609-622, 1989.
8. Y. Chen, "Nonlinear yaw card data reduction," System Engineering and Electronic Techniques, vol. 1991, no. 3, pp. 53-58, 1991 (in Chinese).
9. D. J. Linse and R. F. Stengel, "Identification of aerodynamic coefficients using computational neural networks," J. Guidance, Contr. and Dynamics, vol. 16, no. 6, pp. 1018-1025, 1994.
10. Y. Chen and H. Dou, "Researches on the optimal control solution of identifying fitting drag coefficient curve from radar measured velocity data," Aerodynamic Experiment and Measurement Contr., vol. 1993, no. 2, pp. 81-89, 1993 (in Chinese).
11. _, "Data fitting algorithm and general purpose software by constrained multistaged polynomials with different orders," Aerodynamic Experiment and Measurement Contr., vol. 5, no. 3, pp. 78-86, 1991 (in Chinese).
12. Y. Chen, C. Wen, Z. Gong, and M. Sun, "Drag coefficient curve identification of projectiles from flight tests via optimal dynamic fitting," J. Contr. Eng. Practice, vol. 5, no. 5, pp. 627-636, May 1997.
13. S. Arimoto, S. Kawamura, and F. Miyazaki, "Bettering operation of robots by learning," J. Robotic Syst., vol. 1, no. 2, pp. 123-140, 1984.
14. Z. Bien and K. M. Huh, "High-order iterative learning control algorithm," Proc. Inst. Elect. Eng., vol. 136, pt. D, no. 3, pp. 105-112, 1989.
15. Y. Chen, M. Sun, B. Huang, and H. Dou, "Robust higher order repetitive learning control algorithm for tracking control of delayed repetitive systems," in Proc. 31st IEEE Conf. Decision and Contr., Tucson, AZ, Dec. 1992, pp. 2504-2510.
16. Y. Chen, "Researches on trajectory prediction models and software for spin-stabilized projectiles (I), (II), (III)," Projectile and Rocket Fascicule of Acta Armamentarii, vol. 1990, no. 3, pp. 1-7;
17. Y. Chen, Projectile and Rocket Fascicule of Acta Armamentarii, vol. 1990, no. 4, pp. 1-11, 1990;
18. Y. Chen, Projectile and Rocket Fascicule of Acta Armamentarii, vol. 1991, no. 1, pp. 1-10, 1991 (in Chinese).