Optimal Guidance and Its Applications in Missiles and UAVs

£139.50

Optimal Guidance and Its Applications in Missiles and UAVs

Automatic control engineering Aerospace and aviation technology Astronautics Artificial intelligence

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

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Collection: Springer Aerospace Technology

Language: English

Published by: Springer

Published on: 13th May 2020

Format: LCP-protected ePub

Size: 14 Mb

ISBN: 9783030473488


Overview

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.

Concept of Optimal Guidance

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.

Applications and Insights

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.

Practical Importance

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.

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