Advances in Aerospace Systems Dynamics and Control Systems: - download pdf or read online

By Cornelius T. Leondes

ISBN-10: 0120127326

ISBN-13: 9780120127320

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Extra resources for Advances in Aerospace Systems Dynamics and Control Systems: Advances in Theory and Applications : Advances in Aerospace Systems Dynamics and Control Systesm, Part 2 of 3

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DE VILLIERS, "Proportional Navigation and the Game of Two Cars," Tech. Rep. TWISK 544, NRIMS, CSIR, Pretoria, July 1987. 10. R. ISAACS, "Differential Games," Wiley, New York, 1965. 11. Y. YAVIN and R. DE VILLIERS, "The Game of Two Cars with a Containment Probability as a Cost Function: The Case of Variable Speed," Comput. Math. Appl. 18, 61-67 (1989). 12. Y. YAVIN and R. DE VILLIERS, Proportional Navigation and the Game of Two Cars: The Case of a Pursuer with Variable Speed," Comput. Math. Appl.

SIMS and R. B. ASHER, "Optimal and Suboptimal Results in Full and Reduced-Order Linear Filtering," IEEE Trans. Autom. Control AC-23, 469-472 (1978). 38 WASSIM M. HADDAD AND DENNIS S. BERNSTEIN 8. F. W. FAIRMAN and R. D. GUPTA, "Design of Multi-functional Reduced-Order Observers," Int. J. Syst. Sei. 11, 1083-1094 (1980). 9. C. S. SIMS and L. G. STOTTS, "Linear Discrete Reduced-Order Filtering," Proc. IEEE Conf. Decision Control, 1172-1177 (1979). 10. T. E. FORTMAN and D. WILLIAMS, "Design of Low-Order Observers for Linear Feedback Control Laws," IEEE Trans.

SUFFICIENT CONDITIONS FOR COMBINED LEAST-SQUARES AND FREQUENCY-DOMAIN ERROR ESTIMATION In this section we combine Lemma 1 with the converse of Theorem 2 to obtain our main result, guaranteeing H^ -constrained estimation with an optimized least-squares bound on the state-estimation error criterion. WASSIM M. HADDAD AND DENNIS S. BERNSTEIN 36 Theorem 3. Suppose there exist 1, 0* eNn satisfying (60) and (61), and let (Ae9 Be, Q,D e ) be given by (56)-(59). Then (48) is satisfied if and only if Ac is asymptotically stable.

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Advances in Aerospace Systems Dynamics and Control Systems: Advances in Theory and Applications : Advances in Aerospace Systems Dynamics and Control Systesm, Part 2 of 3 by Cornelius T. Leondes


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