Optimal guidance and its applications in missiles and UAVs / Shaoming He, Chang-Hun Lee, Hyo-Sang Shin, Antonios Tsourdos.
He, Shaoming.; Lee, Chang-Hun.; Shin, Hyo-Sang.; Tsourdos, Antonios.
2020
UG630
Available Online

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Title Optimal guidance and its applications in missiles and UAVs / Shaoming He, Chang-Hun Lee, Hyo-Sang Shin, Antonios Tsourdos.
Author He, Shaoming.
ISBN 9783030473488 (electronic book)
3030473481 (electronic book)
9783030473471
3030473473
DOI https://doi.org/10.1007/978-3-030-47
https://doi.org/10.1007/978-3-030-47348-8
Publication Details Cham : Springer, 2020.
Language English
Description 1 online resource (221 pages).
Item Number 10.1007/978-3-030-47
10.1007/978-3-030-47348-8 doi
Call Number UG630
Dewey Decimal Classification 623.4/519
Summary 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.
Bibliography, etc. Note Includes bibliographical references.
Access Note Access limited to authorized users.
Digital File Characteristics text file PDF
Source of Description Description based on print version record.
Added Author Lee, Chang-Hun.
Shin, Hyo-Sang.
Tsourdos, Antonios.
Series Springer aerospace technology.
Available in Other Form Optimal Guidance and Its Applications in Missiles and UAVs
Linked Resources Online Access
Record Appears in Online Resources > Ebooks
All Resources
Introduction of Optimal Guidance
Optimality of Error Dynamics in Missile Guidance
Three-Dimensional Optimal Impact-Time-Control Guidance Law
Gravity-Turn Assisted Optimal Guidance Law
Observability-Enhancement Optimal Guidance Law
Optimal Proportional-Integral Guidance Law
Energy-Optimal Waypoint-Following Guidance Law
Conclusions.

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