Optimizing evasive maneuvering of planes using a flight quality driven model

Chang Liu, Shaoshan Sun, Chenggang Tao, Yingxin Shou, Bin Xu

科研成果: 期刊稿件文章同行评审

4 引用 (Scopus)

摘要

This paper investigates the optimal evasive maneuver for a plane to avoid an incoming missile. To accurately model the system dynamics while improving computational efficiency, a simplified plane model based on flight quality is established. A missile model with proportional guidance is also formulated. The problem of determining the optimal evasion plane maneuver is formulated. The Gauss pseudospectral method (GPM) is proposed as a solution to find the optimal maneuver. The optimized maneuver is validated by testing it on a high-fidelity 6-degree-of-freedom (6-DOF) model, which demonstrates the effectiveness of the proposed simplified plane model. The Monte Carlo method is employed to evaluate the capability of the plane to evade missiles in various scenarios and elucidate general principles for successful evasion.

源语言英语
文章编号132206
期刊Science China Information Sciences
67
3
DOI
出版状态已出版 - 3月 2024

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