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Titlebook: Compound Control Methodology for Flight Vehicles; Yuanqing Xia,Mengyin Fu Book 2013 Springer-Verlag Berlin Heidelberg 2013 Active Disturba

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31#
發(fā)表于 2025-3-26 21:03:09 | 只看該作者
Fatigue of Steel Plated Structures,on [130],[196]. The attitude motion of a rigid body is represented by a set of two vector equations, namely, the kinematic equation which relates to the time derivatives of the orientation angles to the angular velocity vector and the dynamic equation which describes the time evolution of the angula
32#
發(fā)表于 2025-3-27 02:29:19 | 只看該作者
33#
發(fā)表于 2025-3-27 06:25:13 | 只看該作者
Steel Structures Design Based on Eurocode 3aws due to the high effectiveness and simple implementation [87, 285, 97, 248]. It is well known that PN is the optimal guidance law with a navigation ratio .?=?3, and it can result in successful interceptions under a wide range of engagement conditions. However, the PN guidance law is more applicab
34#
發(fā)表于 2025-3-27 09:39:36 | 只看該作者
https://doi.org/10.1007/978-981-10-8836-0and simple implementation [299, 332, 221, 7]. Specially, PN guidance laws can be easily applied to many-to-one engagement scenarios and achieve the cooperative simultaneous attack of multiple missiles against their common target [123]. However, the PN guidance law is more applicable for the task of
35#
發(fā)表于 2025-3-27 16:56:17 | 只看該作者
https://doi.org/10.1007/978-1-4471-4872-2increasingly need for the accuracy of missile guidance. While there has been rapid improvement in realizing the physical conditions for high-speed missile guidance and intercepting missiles, various theories in this field are also created. Dated back to 30 years ago, Guelman [89] made a comprehensiv
36#
發(fā)表于 2025-3-27 19:19:46 | 只看該作者
https://doi.org/10.1007/978-3-642-36841-7Active Disturbance Rejection Control (ADRC); Compound Control; Flight Control; Flight Vehicles; Networke
37#
發(fā)表于 2025-3-27 23:38:18 | 只看該作者
38#
發(fā)表于 2025-3-28 05:18:35 | 只看該作者
Yuanqing Xia,Mengyin FuPresents a Compound Control Methodology for Flight Vehicles.Includes overview chapters to flight control, sliding mode control (SMC), active disturbance rejection control (ADRC) and compound control.W
39#
發(fā)表于 2025-3-28 08:29:02 | 只看該作者
Lecture Notes in Control and Information Scienceshttp://image.papertrans.cn/c/image/231858.jpg
40#
發(fā)表于 2025-3-28 10:51:27 | 只看該作者
Overview of ADRC,ever, with the development of science and technology, the requirements of control system focus on control accuracy and rapid respond speed, and the increasingly high demands ability to adapt to the changes in the environment, then the classical PID can not obtain satisfied control performance with some shortcomings.
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