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2020 | OriginalPaper | Chapter

1. Introduction of Optimal Guidance

Authors : Shaoming He, Chang-Hun Lee, Hyo-Sang Shin, Antonios Tsourdos

Published in: Optimal Guidance and Its Applications in Missiles and UAVs

Publisher: Springer International Publishing

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Abstract

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.

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next chapter Optimal Error Dynamics in Missile Guidance
Literature
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Metadata
Title
Introduction of Optimal Guidance
Authors
Shaoming He
Chang-Hun Lee
Hyo-Sang Shin
Antonios Tsourdos
Copyright Year
2020
Book
Optimal Guidance and Its Applications in Missiles and UAVs

Print ISBN: 978-3-030-47347-1

Electronic ISBN: 978-3-030-47348-8

Copyright Year: 2020

DOI
https://doi.org/10.1007/978-3-030-47348-8_1

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