Impact time and angle guidance strategy with maximum lateral acceleration constraints:Theory and experimentOA
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
School of Artificial Intelligence,Beihang University,Beijing 100191,ChinaSchool of Artificial Intelligence,Beihang University,Beijing 100191,ChinaSchool of Automation Science and Electrical Engineering,Science and Technology on Aircraft Control Laboratory,Beihang University,Beijing 100191,ChinaSchool of Automation Science and Electrical Engineering,Science and Technology on Aircraft Control Laboratory,Beihang University,Beijing 100191,ChinaSchool of Astronautics,Beihang University,Beijing 100191,ChinaSchool 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
Bézier trajectory shapingImpact angle guidanceImpact time controlParameter optimizationTrajectory tracking
Bézier trajectory shapingImpact angle guidanceImpact time controlParameter optimizationTrajectory tracking
《中国航空学报（英文版）》 2026 (7)
47-63,17
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).
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