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Time-optimal guidance for intercepting moving targets with impact-angle constraints 被引量:3

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摘要 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.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2022年第7期157-167,共11页 中国航空学报(英文版)
基金 supported by the National Natural Science Foundation of China(Nos.61903331,62088101) the Shanghai Aerospace Science and Technology Innovation Fund,China(No.SAST2019-10)。
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