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Optimal Guidance and Its Applications in Missiles and UAVs

  • Book
  • © 2020

Overview

  • 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 demonstrate the effectiveness of the proposed formulation and validate the analytic findings
  • Paves the way for future research in the domain of aerospace guidance

Part of the book series: Springer Aerospace Technology (SAT)

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Table of contents (10 chapters)

  1. Optimal Guidance in Missile Applications

  2. Optimal Guidance in UAV Applications

Keywords

About this book

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.

Authors and Affiliations

  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China

    Shaoming He

  • Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon, Korea (Republic of)

    Chang-Hun Lee

  • Aerospace, Transport and Manufacturing, Cranfield University, Cranfield, UK

    Hyo-Sang Shin, Antonios Tsourdos

Bibliographic Information

  • Book Title: Optimal Guidance and Its Applications in Missiles and UAVs

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

  • Series Title: Springer Aerospace Technology

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

  • Publisher: Springer Cham

  • eBook Packages: Engineering, Engineering (R0)

  • Copyright Information: The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerland AG 2020

  • Hardcover ISBN: 978-3-030-47347-1Published: 14 May 2020

  • Softcover ISBN: 978-3-030-47350-1Published: 14 May 2021

  • eBook ISBN: 978-3-030-47348-8Published: 13 May 2020

  • Series ISSN: 1869-1730

  • Series E-ISSN: 1869-1749

  • Edition Number: 1

  • Number of Pages: XIII, 214

  • Number of Illustrations: 2 b/w illustrations, 47 illustrations in colour

  • Topics: Aerospace Technology and Astronautics, Control, Robotics, Mechatronics, Computational Intelligence

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