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Impact time and angle guidance strategy with maximum lateral acceleration constraints:Theory and experiment

Heng LI Xiaokang LÜ Jianglong YU Qing WANG Kun ZHANG Xiwang DONG

中国航空学报（英文版）2026，Vol.39Issue(7)：47-63,17.

中国航空学报（英文版）2026，Vol.39Issue(7)：47-63,17.DOI:10.1016/j.cja.2025.103775

Impact time and angle guidance strategy with maximum lateral acceleration constraints:Theory and experiment

Heng LI ¹Xiaokang LÜ ¹Jianglong YU ²Qing WANG ²Kun ZHANG ³Xiwang DONG⁴

作者信息

1. School of Artificial Intelligence,Beihang University,Beijing 100191,China
2. School of Automation Science and Electrical Engineering,Science and Technology on Aircraft Control Laboratory,Beihang University,Beijing 100191,China
3. School of Astronautics,Beihang University,Beijing 100191,China
4. School of Artificial Intelligence,Beihang University,Beijing 100191,China||School of Automation Science and Electrical Engineering,Science and Technology on Aircraft Control Laboratory,Beihang University,Beijing 100191,China||Institute of Unmanned System,Beihang University,Beijing 100191,China
折叠

摘要

关键词

Bézier trajectory shaping/Impact angle guidance/Impact time control/Parameter optimization/Trajectory tracking

Key words

Bézier trajectory shaping/Impact angle guidance/Impact time control/Parameter optimization/Trajectory tracking

引用本文复制引用

Heng LI,Xiaokang LÜ,Jianglong YU,Qing WANG,Kun ZHANG,Xiwang DONG..Impact time and angle guidance strategy with maximum lateral acceleration constraints:Theory and experiment[J].中国航空学报（英文版）,2026,39(7):47-63,17.

基金项目

This work was supported by the National Natural Science Foundation of China(Nos.62473029 and U2241217),the Fundamental Research Funds for the Central Universities,China(No.501XYGG2025103012),and the Postdoctoral Fel-lowship Program of CPSF,China(No.BX20240462). （Nos.62473029 and U2241217）

中国航空学报（英文版）

ISSN：1000-9361

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