说明
发表于 2025-3-23 12:01:34
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尊敬
发表于 2025-3-23 15:11:23
,Mesure de Hausdorff de la trajectoire de certains processus à accroissements indépendants et statio
粗野
发表于 2025-3-23 19:46:47
,Une démonstration simple du théorème de R. M. Dudley et Marek Kanter sur les lois Zéro-un pour les
conspicuous
发表于 2025-3-24 00:18:28
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GENUS
发表于 2025-3-24 06:12:34
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离开真充足
发表于 2025-3-24 07:27:49
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蘑菇
发表于 2025-3-24 14:05:30
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
发表于 2025-3-24 15:31:47
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
直言不讳
发表于 2025-3-24 20:36:33
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
发表于 2025-3-25 00:54:50
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