Titlebook: Mechanics and Control; Proceedings of the 4 Janislaw M. Skowronski,Henryk Flashner,Ramesh S. G Conference proceedings 1992 Springer-Verlag

Limousine

天文臺(tái)

0170-8643 17papers containing original and recent work of the partici-pants developed in 3 basic directions: feed-back control ofuncertain systems,flexible mechanical structures and flightcontrol.978-3-540-54954-3978-3-540-46606-2Series ISSN 0170-8643 Series E-ISSN 1610-7411

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FEAS

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Self-Help-Group

Controllability of a Forkker-Planck equation, the Schrodinger system, and a related stochastic optimison, under proper assumptions. Theorem 2 gives a sufficiency condition concerning the given initial and terminal data for that solution to exist. Theorem 3 states that v* is an optimal feedback control for a stochastic optimal control problem with constraint on the end-state, termed ., and further

車床

Stability robustness of linear feedback controlled flexible mechanical systems,ng controller is designed based on a rigidified model, i.e., a model in which some of the flexible components are assumed rigid, it is not true that this controller also stabilizes the ‘real’ flexible system. We present a condition which guarantees that a stabilizing controller whose design is based

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Predictive controller and estimator for nasa deep space network antennas,e control law. This approach has been used for the design of tracking controllers for the NASA/JPL 70-m antennas. Several tracking scenarios have been tested (step input, constant rate rise and fall, raised cosine trajectory), and significant improvement of performance has been observed. A wider ban

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免費(fèi)

Observers for controllers with matched uncertainty in A, B and C matrices,s, is assumed to satisfy certain matching conditions. Lyapunov techniques are used to establish sufficient condition for stability for a given uncertainty bound. In particular, sufficient conditions are obtained that, if met, guarantee stabilization regardless of the size of the uncertainty.