Introduction of Optimal Guidance

Shaoming He; Chang Hun Lee; Hyo Sang Shin; Antonios Tsourdos

doi:10.1007/978-3-030-47348-8_1

Introduction of Optimal Guidance

Shaoming He^*, Chang Hun Lee, Hyo Sang Shin, Antonios Tsourdos

^*此作品的通讯作者

宇航学院

科研成果: 书/报告/会议事项章节 › 章节 › 同行评审

1 引用（Scopus）

摘要

Guidance is one of the key parts of modern aerospace vehicles since it enables improved autonomy by guiding the vehicle to approach a specific stationary/dynamic position. Optimal control theory is known as a valuable and systematic tool in the design and development of guidance algorithms. We explore 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.

源语言	英语
主期刊名	Springer Aerospace Technology
出版商	Springer Nature
页	1-6
页数	6
DOI	https://doi.org/10.1007/978-3-030-47348-8_1
出版状态	已出版 - 2020

出版系列

姓名	Springer Aerospace Technology
ISSN（印刷版）	1869-1730
ISSN（电子版）	1869-1749

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10.1007/978-3-030-47348-8_1

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He, S., Lee, C. H., Shin, H. S., & Tsourdos, A. (2020). Introduction of Optimal Guidance. 在 Springer Aerospace Technology (页码 1-6). (Springer Aerospace Technology). Springer Nature. https://doi.org/10.1007/978-3-030-47348-8_1

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Introduction of Optimal Guidance

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