Impact time control guidance against maneuvering targets based on a nonlinear virtual relative model

Yuru BIN, Hui WANG*, Defu LIN, Yaning WANG, Xin SUN

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

8 引用 (Scopus)

摘要

Aiming at the problem of high-precision interception of air-maneuvering targets with impact time constraints, this paper proposes a novel guidance law based on a nonlinear virtual relative model in which the origin is attached to the target. In this way, the original maneuvering target is transformed into a stationary one. A polynomial function of the guidance command in the range domain with two unknown coefficients is introduced into the virtual model, one of the coefficients is determined to achieve the impact time constraint, and the other is determined to satisfy a newly defined virtual look angle constraint. For meeting the terminal constraints simultaneously, the guidance command can finally be obtained. The resulting solution is represented as a combination of proportional navigation guidance-like term which is aimed to meet the zero miss distance constraint, a bias term for impact time control by adjusting the length of the homing trajectory, and an additional term for target maneuvers. Numerous simulations demonstrate that the proposed law achieves an acceptable impact time error for various initial conditions against different types of maneuvering targets and shows more effective performance in comparison with those of other existing guidance laws.

源语言英语
页(从-至)444-459
页数16
期刊Chinese Journal of Aeronautics
36
7
DOI
出版状态已出版 - 7月 2023

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