Two-degree-of-freedom ℋ∞ robust controller for a flexible missile

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 3, 1998, Pages 518-520

  George, K Koshy ^a,b   Bhat, M Seetharama ^a,c  

^a INDIAN INSTITUTE OF SCIENCE   (India)

^b Seoul National University   (South Korea)

^c Department of Aerospace Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85008310817     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.7610     Document Type: Article

References (5)

1. Kreisselmeier, G., and Steinhauser, R., "Systematic Control Design by Optimizing a Vector Performance Index," Proceedings of the International Federation of Automatic Control Symposium on Computer Aided Design of Control Systems (Zürich, Switzerland), Pergamon, Oxford, England, UK, 1980, pp. 113-117.
2. ∞ Norm Bound and Relations to Risk Sensitivity," Systems and Control Letters, Vol. 11, No. 3, 1988, pp. 167-172.
3. ∞-Based Robust Controller for Aerospace Vehicles," Ph.D. Thesis, Dept. of Aerospace Engineering, Indian Inst. of Science, Bangalore, India, Nov. 1996.
4. Horowitz, I. M., Synthesis of Feedback Systems, Academic, New York, 1963, Chap. 6.
5. Safonov, M. G., and Chiang, R.Y., "A Schur Method for Balanced Model Reduction," Proceedings of the 1988 American Control Conference (Atlanta, GA), American Automatic Control Council, 1988, pp. 1036-1040.