Introduction of Optimal Guidance

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

*此作品的通讯作者

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
1-6
页数6
DOI
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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