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Open Access

Time-optimal guidance for intercepting moving targets with impact-angle constraints

Yuan ZHENGaZheng CHENa,b( )Xueming SHAOa,bWenjie ZHAOa
School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China
State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, Hangzhou 310027, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

The minimum-time path for intercepting a moving target with a prescribed impact angle is studied in the paper. The candidate paths from Pontryagin’s maximum principle are synthesized, so that each candidate is related to a zero of a real-valued function. It is found that the real-valued functions or their first-order derivatives can be converted to polynomials of at most fourth degree. As a result, each candidate path can be computed within a constant time by embedding a standard polynomial solver into the typical bisection method. The control strategy along the shortest candidate eventually gives rise to the time-optimal guidance law. Finally, the developments of the paper are illustrated and verified by three numerical examples.

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Chinese Journal of Aeronautics
Pages 157-167

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Cite this article:
ZHENG Y, CHEN Z, SHAO X, et al. Time-optimal guidance for intercepting moving targets with impact-angle constraints. Chinese Journal of Aeronautics, 2022, 35(7): 157-167. https://doi.org/10.1016/j.cja.2021.08.002

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Received: 01 March 2021
Revised: 26 April 2021
Accepted: 01 August 2021
Published: 16 September 2021
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).