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標(biāo)題: Titlebook: On-Orbit Operations Optimization; Modeling and Algorit Leping Yang,Yanwei Zhu,Yuanwen Zhang Book 2014 Leping Yang, Yanwei Zhu, Xianhai Ren, [打印本頁]

作者: malignant    時間: 2025-3-21 18:30
書目名稱On-Orbit Operations Optimization影響因子(影響力)




書目名稱On-Orbit Operations Optimization影響因子(影響力)學(xué)科排名




書目名稱On-Orbit Operations Optimization網(wǎng)絡(luò)公開度




書目名稱On-Orbit Operations Optimization網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱On-Orbit Operations Optimization被引頻次




書目名稱On-Orbit Operations Optimization被引頻次學(xué)科排名




書目名稱On-Orbit Operations Optimization年度引用




書目名稱On-Orbit Operations Optimization年度引用學(xué)科排名




書目名稱On-Orbit Operations Optimization讀者反饋




書目名稱On-Orbit Operations Optimization讀者反饋學(xué)科排名





作者: cataract    時間: 2025-3-21 23:27
On-Orbit Operations Optimization978-1-4939-0838-7Series ISSN 2190-8354 Series E-ISSN 2191-575X
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SpringerBriefs in Optimizationhttp://image.papertrans.cn/o/image/701325.jpg
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作者: 舊病復(fù)發(fā)    時間: 2025-3-22 10:53
Leping Yang,Yanwei Zhu,Yuanwen ZhangReflects the latest progress on modeling and algorithms of on-orbit operation optimization.Offers a comprehensive presentation of the features and classifications of on-orbit operations optimization,
作者: 拔出    時間: 2025-3-22 15:18
2190-8354 lation cases that address problems in these four categories. This text will serve as a quick reference for engineers, graduate students, postgraduates in the fields of optimization research and on-orbit operation mission planning.978-1-4939-0837-0978-1-4939-0838-7Series ISSN 2190-8354 Series E-ISSN 2191-575X
作者: Saline    時間: 2025-3-22 20:12
Multi-Spacecraft Coordinated Planning, for coordinated trajectory planning, illustrated by cases of constrained circular flyaround, natural elliptical flyaround, flyaround with different orbit, and cubic flyaround. Then, considering on-orbit operations attitude requirements, the contraction theory is applied to 6-DOF synchronized control, illustrated by a four-spacecraft cluster case.
作者: obeisance    時間: 2025-3-23 00:47
Book 2014g. The authors then formulate models, introduce optimization methods, and investigate simulation cases that address problems in these four categories. This text will serve as a quick reference for engineers, graduate students, postgraduates in the fields of optimization research and on-orbit operation mission planning.
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Proximity Relative Motion Planning,mproved Artificial Potential Function (IAPF) is applied to surface following trajectory optimization when the field of view (FOV) is blocked. For a maneuvered customer, the Inverse Dynamics in the Virtual Domain method (IDVD) is explored to approach online trajectory planning.
作者: contradict    時間: 2025-3-23 17:36
Introduction,cope repairs, assembly of the International Space Station, as well as demonstration of the Orbital Express, the growing importance of On-Orbit Servicing (OOS) has been emphasized. OOS, which has grown to be a hot topic in on-orbit operations field, will help transit space utilization into a new era of operational efficiency and cost-effectiveness.
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Spacecraft Multi-Mission Planning,ecraft multi-mission planning is founded on one-to-one single mission planning, including far-range orbital maneuver planning and proximity relative motion planning. In this chapter, a multilevel nonlinear planning model, which can be simplified as mission assignment, sequence arrangement, and time
作者: 棲息地    時間: 2025-3-24 12:21
Far-Range Orbital Maneuver Planning,omer until the former gets close to the latter. Then the servicer sensor captures the customer, which marks the beginning of proximity relative motion phase. Trajectory planning of far-range orbital maneuver is to optimize the orbital maneuver for the servicer under the constraints of time, fuel, an
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Multi-Spacecraft Coordinated Planning,atellites, which requires coordinated planning to achieve and keep a desired configuration. The cyclic pursuit method and the contraction theory are investigated due to their promising features, such as less information exchange and global convergence. First, the cyclic pursuit method is put forward
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