带撞击角约束的静止目标最佳制导法参数化解决方案

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-11-19 DOI:10.1109/TAES.2024.3501996
Yiji Zhu;Cong Zhou;Sai Chen;Xun Song;Kebo Li;Chaoyong Li
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引用次数: 0

摘要

提出了一种具有冲击角约束的针对静止目标的三维参数化制导律。特别地,我们对旋转视距框架内的相对运动进行了降维处理,并将最优制导问题转化为几何参数化问题,将状态变量和伴随状态变量参数化为非均匀三次b样条,然后给出了确定其最优值的数值解。仿真结果验证了所提制导律的有效性,并验证了所提参数法的计算效率优于已建立的高斯伪谱法。
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A Parameterized Solution to Optimal Guidance Law Against Stationary Target With Impact Angle Constraint
A 3-D parameterized guidance law against stationary target with impact angle constraint is proposed in this article. In particular, we perform a dimension reduction on the relative motion in the rotating line-of-sight frame, and proceed to formulate the optimal guidance problem into a geometric parameterization problem, with the state and costate variables parameterized as nonuniform cubic B-Spline, and subsequently, proposed a numerical solution to determine its optimal value. Simulation results demonstrate the effectiveness of the proposed guidance law, and verified that the computational efficiency of the proposed parametric method outperforms that of the well-established Gauss pseudospectral method.
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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