標(biāo)題: Titlebook: Optimal Guidance and Its Applications in Missiles and UAVs; Shaoming He,Chang-Hun Lee,Antonios Tsourdos Book 2020 The Editor(s) (if applic [打印本頁(yè)] 作者: 高出來(lái)的名詞 時(shí)間: 2025-3-21 17:37
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作者: Liability 時(shí)間: 2025-3-21 23:18
1869-1730 ce and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority..978-3-030-47350-1978-3-030-47348-8Series ISSN 1869-1730 Series E-ISSN 1869-1749 作者: 鉤針織物 時(shí)間: 2025-3-22 03:02
Shaoming He,Chang-Hun Lee,Hyo-Sang Shin,Antonios Tsourdos作者: 有其法作用 時(shí)間: 2025-3-22 08:20
Shaoming He,Chang-Hun Lee,Hyo-Sang Shin,Antonios Tsourdos作者: PANG 時(shí)間: 2025-3-22 08:57
Shaoming He,Chang-Hun Lee,Hyo-Sang Shin,Antonios Tsourdos作者: 絕緣 時(shí)間: 2025-3-22 13:36 作者: 集聚成團(tuán) 時(shí)間: 2025-3-22 20:36
Shaoming He,Chang-Hun Lee,Hyo-Sang Shin,Antonios Tsourdos作者: legacy 時(shí)間: 2025-3-23 00:15 作者: crescendo 時(shí)間: 2025-3-23 01:30 作者: 砍伐 時(shí)間: 2025-3-23 08:40
Shaoming He,Chang-Hun Lee,Hyo-Sang Shin,Antonios Tsourdos作者: 有偏見(jiàn) 時(shí)間: 2025-3-23 11:54
Shaoming He,Chang-Hun Lee,Hyo-Sang Shin,Antonios Tsourdoschoice of geometric and symbolic transformations that are necessary to achieve a particular visualization. Designers of map-like visualizations are thus challenged to seriously consider the implications of particular computational techniques and the consequences of symbolization choices.作者: extemporaneous 時(shí)間: 2025-3-23 17:17 作者: Buttress 時(shí)間: 2025-3-23 21:49
Book 2020e laws. In practice, this information is important in ensuring confidence in the performance and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority..作者: Essential 時(shí)間: 2025-3-24 00:20 作者: GRIEF 時(shí)間: 2025-3-24 04:08 作者: 樂(lè)器演奏者 時(shí)間: 2025-3-24 07:31
Optimal Guidance and Its Applications in Missiles and UAVs作者: Ingrained 時(shí)間: 2025-3-24 13:07 作者: 金絲雀 時(shí)間: 2025-3-24 18:51
Optimal Error Dynamics in Missile Guidanceptimal error dynamics for guidance law design to achieve various operational objectives. The proposed optimal error dynamics is derived by solving a linear quadratic optimal control problem through Schwarz’s inequality approach. The properties of the proposed optimal error dynamics are discussed. Th作者: 用樹皮 時(shí)間: 2025-3-24 19:43
Optimal Trajectory Shaping Guidance Law with Seeker’s Field-of-View ConstraintThe proposed guidance law is derived by using the concept of biased PNG (BPNG). The guidance law developed leverages a nonlinear function to ensure the boundedness of velocity lead angle to cater for seeker’s FOV constraint. The finite-time convergence of the impact time error and impact angle error作者: 安裝 時(shí)間: 2025-3-25 00:19 作者: pacific 時(shí)間: 2025-3-25 05:22
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作者: abracadabra 時(shí)間: 2025-3-25 08:30 作者: 火車車輪 時(shí)間: 2025-3-25 12:42
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作者: mitten 時(shí)間: 2025-3-25 16:45 作者: 無(wú)意 時(shí)間: 2025-3-25 23:24 作者: Fulsome 時(shí)間: 2025-3-26 02:51 作者: 使腐爛 時(shí)間: 2025-3-26 06:04 作者: Confirm 時(shí)間: 2025-3-26 08:37 作者: 逢迎春日 時(shí)間: 2025-3-26 16:27
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作者: CRUDE 時(shí)間: 2025-3-26 17:52 作者: Gene408 時(shí)間: 2025-3-26 23:32
Optimal Guidance and Its Applications in Missiles and UAVs978-3-030-47348-8Series ISSN 1869-1730 Series E-ISSN 1869-1749 作者: hair-bulb 時(shí)間: 2025-3-27 01:25
Shaoming He,Chang-Hun Lee,Antonios TsourdosProvides a valuable resource for engineers working on optimal guidance and control systems, as well as graduate students majoring in aerospace engineering.Presents numerical simulations that clearly d作者: 披肩 時(shí)間: 2025-3-27 08:20 作者: RAGE 時(shí)間: 2025-3-27 13:30
https://doi.org/10.1007/978-3-030-47348-8Missile Guidance; Guidance Law; aerospace engineering; aerospace vehicles; unmanned aerial vehicles; traj作者: nerve-sparing 時(shí)間: 2025-3-27 17:38 作者: 形容詞 時(shí)間: 2025-3-27 21:17
Introduction of Optimal Guidance,re the characteristics of classical proportional navigation guidance and present the motivation of the development of new optimal guidance laws in this chapter. The overall aim of this book is then summarized and the organization of the entire book, together with some highlights of each chapter, are presented.作者: 混合物 時(shí)間: 2025-3-27 22:00
Minimum-Effort Waypoint-Following Guidance Law laws developed can be applied to general waypoint-following missions with an arbitrary number of waypoints and an arbitrary number of arrival angle constraints. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed formulations.作者: 有花 時(shí)間: 2025-3-28 02:52 作者: Preserve 時(shí)間: 2025-3-28 09:35
Optimal Trajectory Shaping Guidance Law with Seeker’s Field-of-View Constraint is theoretically analyzed. By investigating the optimality of the biased command, the physical meaning of the proposed trajectory shaping guidance law is revealed to support practical applications. Numerical simulations clearly demonstrate the effectiveness of the proposed formulation.作者: 臥虎藏龍 時(shí)間: 2025-3-28 10:45 作者: GRACE 時(shí)間: 2025-3-28 14:57 作者: synovium 時(shí)間: 2025-3-28 21:14
Energy-Optimal Waypoint-Following Guidance Law Considering Autopilot DynamicsTheoretical analysis reveals that previously suggested optimal point-to-point guidance laws are special cases of the proposed approach. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed formulations.作者: Jacket 時(shí)間: 2025-3-29 01:23 作者: CLAP 時(shí)間: 2025-3-29 03:27
Gravity-Turn-Assisted Optimal Guidance Lawsed guidance law lies in that it ensures zero final guidance command and enables energy saving with the aid of utilizing gravity turn. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed approach.作者: abreast 時(shí)間: 2025-3-29 08:39
10樓作者: 地名表 時(shí)間: 2025-3-29 11:39
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