哈尔滨工业大学学报（英文版）2003，Vol.10Issue(4)：443-446,4.
Design of MGA trajectories for main belt asteroid
Design of MGA trajectories for main belt asteroid
崔祜涛 1乔栋 1崔平远 1栾恩杰2
作者信息
- 1. Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin 150001, China
- 2. China National Space Administration, Beijing 100037, China
- 折叠
摘要
Abstract
Asteroid exploration is one of the most sophisticated missions currently being investigated. Gravityassist trajectories have proven valuable in interplanetary missions such as the Pioneer, Voyager and Galileo. In this paper, we design interplanetary trajectory for main belt asteroid exploration mission with the Mars gravityassist (MGA) using "pork chop" plots and patched-conic theory and give some initial valuable trajectory parameters on main belt asteroid exploration mission with MGA.关键词
Design trajectory/Gravity assist trajectory/Rendezvous with asteroidKey words
Design trajectory/Gravity assist trajectory/Rendezvous with asteroid分类
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崔祜涛,乔栋,崔平远,栾恩杰..Design of MGA trajectories for main belt asteroid[J].哈尔滨工业大学学报（英文版）,2003,10(4):443-446,4.
