Titlebook: Séminaire de Probabilités VIII; Université de Strasb C. Dellacherie,P.A. Meyer,M. Weil Conference proceedings 1974 Springer-Verlag GmbH Ger

說明

尊敬

,Mesure de Hausdorff de la trajectoire de certains processus à accroissements indépendants et statio

粗野

,Une démonstration simple du théorème de R. M. Dudley et Marek Kanter sur les lois Zéro-un pour les

conspicuous

GENUS

離開真充足

蘑菇

J. Bretagnollell be directly guaranteed in the control design. Moreover, this book systematically proposes a series of spacecraft performance guaranteed control algorithms based on the practical situation of the aerospace system. For individual spacecraft, control algorithms that consider practical problems such

ventilate

K. L. Chungthe command filter. This filter can constrain the signal’s rate, magnitude/amplitude, and bandwidth, smooth the command signals and avoid peak interference. In this way, the response of the actuators is closer to the theoretical design. The spacecraft attitude tracking closed-loop system can not onl

直言不諱

C. Dellacherieaxed through the more precise settling time design. Simultaneously, the finite-time algorithm also improves the transient performance of the system, such as the smoother state trajectory, etc. Under the proposed control algorithms, the transient and steady-state behaviors of the spacecraft attitude

THROB

C. Dellacherie basic form and framework of the performance guaranteed control algorithm studied in this book, including the performance guaranteed constraint function, fundamental error transformation, performance constraint auxiliary variable, virtual auxiliary system, disturbance suppression, control algorithm