利用径向力平衡飞行控制的航天器高精度轨道捕获方法.

Autor: 孟云鹤, 侯佳睿, 罗宇飞
Zdroj: Journal of National University of Defense Technology / Guofang Keji Daxue Xuebao; Mar2024, Vol. 46 Issue 2, p27-35, 9p
Databáze: Complementary Index