| 引用本文: | 程志强,闫星辉,张帆,朱纪洪.一种变速度条件下控制攻击角度和时间的制导律[J].控制理论与应用,2024,41(2):364~372.[点击复制] |
| CHENG Zhi-qiang,Yan Xing-hui,Zhang Fan,Zhu Ji-hong.An impact time and angle control guidance law under variable speed condition[J].Control Theory and Technology,2024,41(2):364~372.[点击复制] |
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| 一种变速度条件下控制攻击角度和时间的制导律 |
| An impact time and angle control guidance law under variable speed condition |
| 摘要点击 2559 全文点击 130 投稿时间：2022-07-23 修订日期：2023-12-10 |
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| DOI编号 10.7641/CTA.2023.20660 |
| 2024,41(2):364-372 |
| 中文关键词 攻击角度 攻击时间 变速度 轨迹设计 贝塞尔曲线 |
| 英文关键词 impact angle impact time variable speed trajectory design bezier curve |
| 基金项目 |
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| 中文摘要 |
| 对攻击角度和时间进行控制, 可以使得多枚导弹按照特定的角度和时间对目标进行打击, 在军事上有广泛的应用前景. 目前已有控制攻击角度和时间的制导律极少考虑速度变化的情况, 在实际运用中具有较大的局限性.本文基于贝塞尔曲线加直线的二段式轨迹, 首先分析并证明了该轨迹长度和最大曲率的变化规律, 在此基础上, 通过二分法确定初始轨迹, 针对飞行过程中的诱导阻力和其它扰动, 设计了Bezier-PI控制算法, 通过动态调整轨迹长度来实现攻击时间的高精度控制. 该制导算法计算量小, 鲁棒性强, 适用于弹载计算机实时计算. 通过仿真实验, 验证了该算法可以高精度的控制攻击时间以及攻击角度 |
| 英文摘要 |
| Impact-time-and-angle-control guidance (ITACG) law can realize that multiple missiles strike from different impact angles at the same time, which has a wide range of military applications. However, the current methods to solve the ITACG problem rarely consider the variable speed which will cause great limitations in practical application. Based on the two-segment trajectory of Bezier curve and straight line, we analyze the pattern of maximum curvature of the trajectory, and prove that the trajectory length is monotonic with straight-line length. Second, this paper uses binary search to determine the whole trajectory. Third, to control the impact time, we design a Bezier-PI controller that dynamically adjusts the straightline length. The guidance algorithm has small calculation and strong robustness, which is suitable for real-time calculation by missile-borne computers. The simulation results verified that the algorithm has strong robustness to the induced drag and parasite drag disturbance and can reach a high precision impact time and impact angle. |
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