| 書目名稱 | Optimal Guidance and Its Applications in Missiles and UAVs |
| 編輯 | Shaoming He,Chang-Hun Lee,Antonios Tsourdos |
| 視頻video | http://file.papertrans.cn/703/702882/702882.mp4 |
| 概述 | Provides 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 |
| 叢書名稱 | Springer Aerospace Technology |
| 圖書封面 |  |
| 描述 | .This book presents a comprehensive overview of the recent advances in the domain of optimal guidance, exploring the characteristics of various optimal guidance algorithms and their pros and cons. Optimal guidance is based on the concept of trajectory optimization, which minimizes the meaningful performance index while satisfying certain terminal constraints, and by properly designing the cost function the guidance command can serve as a desired pattern for a variety of mission objectives. The book allows readers to gain a deeper understanding of how optimal guidance law can be utilized to achieve different mission objectives for missiles and UAVs, and also explores the physical meaning and working principle of different new optimal guidance 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.. |
| 出版日期 | Book 2020 |
| 關(guān)鍵詞 | Missile Guidance; Guidance Law; aerospace engineering; aerospace vehicles; unmanned aerial vehicles; traj |
| 版次 | 1 |
| doi | https://doi.org/10.1007/978-3-030-47348-8 |
| isbn_softcover | 978-3-030-47350-1 |
| isbn_ebook | 978-3-030-47348-8Series ISSN 1869-1730 Series E-ISSN 1869-1749 |
| issn_series | 1869-1730 |
| copyright | The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerl |
|Archiver|手機(jī)版|小黑屋|
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