CREEK
发表于 2025-3-23 11:00:15
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CT-angiography
发表于 2025-3-23 17:11:54
https://doi.org/10.1007/978-1-4471-4872-2e study of PN, which is widely considered as a very significant and fundamental theory of missile guidance. Since then, PN guidance law has been complemented and extended. For example, Becker obtained a closed form solution of PN. Ghawghawe et al.
任命
发表于 2025-3-23 21:25:22
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预防注射
发表于 2025-3-24 01:49:35
SMC for Missile Systems Based on Back-Stepping and ESO Techniques,this characteristic, the back-stepping technique is more flexible in designing controllers for high-order nonlinear system models. In the last decade, back-stepping theory has been widely used to solve the transient stabilization problems in missile and flight systems .
言行自由
发表于 2025-3-24 03:21:23
Overview of Flight Vehicle Control,inertia matrix of the spacecraft. The presence of the external disturbance and the inertia uncertainty makes the attitude control problem more complicated. From a practical point of view, the design of efficient and low-cost attitude controllers is an important issue for aerospace industry.
cardiac-arrest
发表于 2025-3-24 06:37:54
Adaptive Nonsingular Terminal SMC for Rigid Spacecraft, spacecraft . investigates the attitude tracking and disturbance rejection problems of spacecraft and converts attitude control into a global stabilization problem. In , some spacecraft-attitude tracking problems are resolved by HOSMC laws.
火车车轮
发表于 2025-3-24 13:58:15
Missile Guidance Law Based on ESO Techniques,le for the task of intercepting a non-maneuvering target or a weakly maneuvering target. In practice, target acceleration can change rapidly. For intercepting a target with powerful maneuvering capability, the performance of PN is degraded and it may be ineffective for some orientations between missile and target.
stroke
发表于 2025-3-24 15:54:07
Missile Guidance Laws Based on SMC and FTC Techniques,intercepting a non-maneuvering target or a weakly maneuvering target. In practice, target acceleration can change rapidly. For intercepting a target with powerful maneuvering capability, the performance of PN is degraded and it may be ineffective for some orientations between missile and target.
忧伤
发表于 2025-3-24 19:01:14
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savage
发表于 2025-3-25 02:36:02
Book 2013nes their advantages and improves the performance of the closed-loop systems. The book is self-contained, providing sufficient mathematical foundations for understanding the contents of each chapter. It will be of significant interest to scientists and engineers engaged in the field of flight vehicle control..