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Published in:
Introduction of Optimal Guidance Read chapter Read first chapter

2020 | OriginalPaper | Chapter

7. Gravity-Turn-Assisted Optimal Intercept Angle Guidance Law

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

This chapter develops a new optimal gravity-turn-assisted intercept angle guidance law for an exo-atmospheric interceptor. The analytical guidance command is derived as a solution of a finite-time optimal regulation problem by using the Lagrange multiplier approach. The convergence of the instantaneous ZEM and intercept angle error is theoretically analyzed based on the instantaneous linear time-invariant system concept. We also reveal that existing optimal impact angle constrained guidance laws are the special cases of the proposed formulation. Numerical simulations with some comparisons clearly demonstrate the effectiveness of the proposed guidance law.

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previous chapter Gravity-Turn-Assisted Optimal Guidance Law
next chapter Minimum-Effort Waypoint-Following Guidance Law
Literature
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He S, Song T, Lin D (2017) Impact angle constrained integrated guidance and control for maneuvering target interception. J Guidance Control Dyn 40(10):2653–2661CrossRef
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Ryoo C-K, Cho H, Tahk M-J (2005) Optimal guidance laws with terminal impact angle constraint. J Guidance Control Dyn 28(4):724–732CrossRef
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Ryoo C-K, Cho H, Tahk M-J (2006) Time-to-go weighted optimal guidance with impact angle constraints. IEEE Trans Control Syst Technol 14(3):483–492CrossRef
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Lee C-H, Tahk M-J, Lee J-I (2013) Generalized formulation of weighted optimal guidance laws with impact angle constraint. IEEE Trans Aerosp Electron Syst 49(2):1317–1322CrossRef
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Seo M-G, Lee C-H, Tahk M-J (2017) New design methodology for impact angle control guidance for various missile and target motions. IEEE Trans Control Syst Technol
Metadata
Title
Gravity-Turn-Assisted Optimal Intercept Angle Guidance Law
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_7

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