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

VER

書目名稱Mechanics and Control影響因子(影響力)




書目名稱Mechanics and Control影響因子(影響力)學(xué)科排名




書目名稱Mechanics and Control網(wǎng)絡(luò)公開度




書目名稱Mechanics and Control網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Mechanics and Control被引頻次




書目名稱Mechanics and Control被引頻次學(xué)科排名




書目名稱Mechanics and Control年度引用




書目名稱Mechanics and Control年度引用學(xué)科排名




書目名稱Mechanics and Control讀者反饋




書目名稱Mechanics and Control讀者反饋學(xué)科排名

富足女人

Conference proceedings 1992d uncertain mechanical sy-tems and promoting application of advanced mechanics in con-trol. The fourth meeting continues the tradition with 17papers containing original and recent work of the partici-pants developed in 3 basic directions: feed-back control ofuncertain systems,flexible mechanical str

Anhydrous

Lyapunov based control design for multiple robots handling a common object,s acting on the object. An adaptive version of the proposed controller is then introduced; the adaptive controller is able to account for the uncertainty in the mass of the load. The convergence analysis of the position, the load mass estimate and the internal forces is also given.

Infusion

On robustness of systems with structured uncertainties,ually conservative. As it is known, often the conservatism is due to the fact that a quadratic form is used as a Lyapunov function. To reduce the conservatism of the bounds we propose to use a piecewise quadratic Lyapunov function. An example demonstrates application of the proposed method.

Aphorism

Reduced-order output feedback control of a class of uncertain systems, noise (with known bound). An output feedback strategy is described which guarantees the existence of a calculable global uniform compact attractor (containing the state origin) for systems of this class.

Vulvodynia

Herpetologist

Stability robustness of linear feedback controlled flexible mechanical systems,re sufficiently stiff. This condition involves the location of the rate sensors and is independent of the location of the displacement sensors. For a natural class of systems and controllers, the condition is automatically satisfied when the rate sensors are collocated with the actuators.

Insul島

BLINK

Optimal trajectories for hypersonic launch vehicles, the energy-state approximation of the equations of motion. The performance objective is a weighted sum of fuel mass and volume, with the weighting factor selected to give minimum gross take-off weight for a specific payload mass and volume.

synovium