pacific 发表于 2025-3-25 05:22:19

Optimal Proportional-Integral Guidance Law ZEM as a new system state, a linear quadratic optimization problem is formulated and then the proposed guidance law is analytically derived through optimal control theory. The closed-form solution of the proposed guidance law is presented to provide better insight of its properties. Additionally, t

abracadabra 发表于 2025-3-25 08:30:16

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火车车轮 发表于 2025-3-25 12:42:02

Gravity-Turn-Assisted Optimal Intercept Angle Guidance Lawmand is derived as a solution of a finite-time optimal regulation problem by using the Lagrange multiplier approach. The convergence of the instantaneous ZEM and intercept angle error is theoretically analyzed based on the instantaneous linear time-invariant system concept. We also reveal that exist

mitten 发表于 2025-3-25 16:45:42

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无意 发表于 2025-3-25 23:24:58

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Fulsome 发表于 2025-3-26 02:51:49

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使腐烂 发表于 2025-3-26 06:04:14

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Confirm 发表于 2025-3-26 08:37:37

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逢迎春日 发表于 2025-3-26 16:27:22

Shaoming He,Chang-Hun Lee,Hyo-Sang Shin,Antonios Tsourdosd Abstract Interpretation (VMCAI 2003), held in New York city, January 9–11, 2003. The purpose of VMCAI was to provide a forum for researchers from three communities—Veri?cation, Model Checking, and Abstract Interpretation—that will facilitate interaction, cross-fertilization, and the advance of hyb

CRUDE 发表于 2025-3-26 17:52:06

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查看完整版本: Titlebook: Optimal Guidance and Its Applications in Missiles and UAVs; Shaoming He,Chang-Hun Lee,Antonios Tsourdos Book 2020 The Editor(s) (if applic