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 |
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Hauptverfasser: | , , , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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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. |
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ISSN: | 1000-9361 |
DOI: | 10.1016/j.cja.2021.08.002 |