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

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...

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Veröffentlicht in:Chinese journal of aeronautics 2022-07, Vol.35 (7), p.157-167
Hauptverfasser: ZHENG, Yuan, CHEN, Zheng, SHAO, Xueming, ZHAO, Wenjie
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Sprache:eng
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Zusammenfassung: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.
ISSN:1000-9361
DOI:10.1016/j.cja.2021.08.002