引用本文: | 张珂洋, 王鹏, 于琦, 等 . 运载火箭助推段大攻角剖面高精度弹道解析解[J]. 北京航空航天大学学报. doi: 10.13700/j.bh.1001-5965.2023.0529 |
Citation: | ZHANG Ke-yang, WANG Peng, YU Qi, et al. Analytical solutions for ascent trajectory under the condition of high angle-of-attack[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0529(in Chinese) |