Robust Control Based on Disturbance Observer and Polynomial Coefficient Approach for Mechanical System

IEEJ Transactions on Industry Applications

Volumn 118, Issue 6, 1998, Pages 707-714

  Miyazaki, Toshimasa ^a   Ohishi, Kiyoshi ^a  

^a NAGAOKA UNIVERSITY OF TECHNOLOGY   (Japan)

Author keywords

Coprime Factorization; Disturbance observer; Polynomial Coefficient Approach; Robust control; Two mass system

Indexed keywords

EID: 84865645420     PISSN: 09136339     EISSN: 13488163     Source Type: Journal    
DOI: 10.1541/ieejias.118.707     Document Type: Article

References (9)

1. K. Ohnishi, M. Shibata and T. Murakami, “Motion Control for Advanced Mechatronics”, IEEE/ASME Trans on Mechatronics, Vol. 1, No. 1, pp. 56-67, 1996.
2. M. Tomizuka, “Model Based Prediction, Preview and Robust Controls in Motion Control Systems”, Proc. of IEEE/IES AMC '96, Vol. 1, pp. 1-6, 1996.
3. Y. Hori, H. Sawada, and Y. Chun, “On Optimal Estimation Speed of Disturbance Observer Used in the Slow Resonance Ratio Control”, Trans. of IEEJ, Vol. 117-D, No. 1, pp. 50-56, 1997.
4. H. Sugimoto, S. Kawasaki, N. Nagata, and E. Watanabe, “One Approach to Speed Control of Two Inertia Resonant System Based on Coprime Factorization Description and its Characteristics”, Trans. of IEEJ, Vol. 114-D, No. 1, pp. 42-50, 1994.
5. S. Morimoto and Y. Takeda, “Two-Degrees-of-Freedom Speed Control of Resonant Mechanical System Based on H∞ Control Theory”, Trans. of IEEJ, Vol. 116-D, No. 1, pp. 65-70, 1996.
6. C. N. Nett, C. A. Jacobson, and M. J. Balas, “A Connection between State-Space and Doubly Coprime Fractional Representations”, IEEE Trans on Automatic Control, Vol. AC-29, No. 9, pp. 831-832, 1984.
7. T. Miyazaki and K. Ohishi, “Design Method of Robust Stable Two-Degrees-of-Freedom Control System Based on Disturbance Observer and Coprime Factorization”, Trans. of IEEJ, Vol. 117-D, No. 5 pp. 572-578, 1997
8. J. C. Doyle, B. A. Francis, A. R. Tannenbaum, “Feedback Control Theory”, New York: Macmillan, 1992.
9. S. Manabe, “Coefficient diagram method as applied to the attitude control of controlled-bias-momentum satellite”, 13th IFAC Symposium on Automatic Control in Aerospace, Palo Alto, California, Sept. 12-16, 1994, pp. 322-327.