摘要 : A novel entry guidance command generation (EGCG) method for hypersonic glide vehicles (HGVs) is proposed in this paper. Apart from the conventional path constraints, terminal constraints, and multiple stationary geographic constra... 展开
作者 | Wang~ Ziyao Tang~ Shengjing Guo~ Jie |
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作者单位 | |
期刊名称 | 《Quality Control, Transactions》 |
页码/总页数 | 1-15 / 15 |
语种/中图分类号 | 英语 / TP3 |
关键词 | Aerodynamics Vehicle dynamics Heuristic algorithms Earth Trajectory planning Mathematical models Licenses Hypersonic glide vehicle entry guidance command generation multiple constraints threats improved artificial potential field |
DOI | 10.1109/ACCESS.2021.3137641 |
馆藏号 | IELEP0398 |