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Erschienen in:
Introduction of Optimal Guidance Kapitel lesen Erstes Kapitel lesen

2020 | OriginalPaper | Buchkapitel

8. Minimum-Effort Waypoint-Following Guidance Law

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

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

Verlag: Springer International Publishing

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Abstract

This chapter addresses the problem of minimum-effort waypoint-following guidance with/without arrival angle constraints of a UAV. By utilizing a linearized kinematics model, the proposed guidance laws are derived as the solutions of a linear quadratic optimal control problem with an arbitrary number of terminal boundary constraints. Theoretical analysis reveals that both optimal proportional navigation guidance and trajectory shaping guidance are special cases of the proposed guidance laws. The key feature of the proposed algorithms lies in their generic property. For this reason, the guidance laws developed can be applied to general waypoint-following missions with an arbitrary number of waypoints and an arbitrary number of arrival angle constraints. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed formulations.

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Vorheriges Kapitel Gravity-Turn-Assisted Optimal Intercept Angle Guidance Law
Nächstes Kapitel Energy-Optimal Waypoint-Following Guidance Law Considering Autopilot Dynamics
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Metadaten
Titel
Minimum-Effort Waypoint-Following Guidance Law
verfasst von
Shaoming He
Chang-Hun Lee
Hyo-Sang Shin
Antonios Tsourdos
Copyright-Jahr
2020
Buch
Optimal Guidance and Its Applications in Missiles and UAVs

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

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

Copyright-Jahr: 2020

DOI
https://doi.org/10.1007/978-3-030-47348-8_8

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